Aircraft Elevator: The Ups and Downs of Flight Explained

Author: Daisy

Jun. 05, 2025

Aircraft Elevator: The Ups and Downs of Flight Explained

Going up? What is the elevator in an aircraft, and how does it work?

An aircraft’s elevator is not the kind you find in a tall building. The elevator on a plane is a movable surface that directly influences pitch control and altitude management. In other words, it is critical in making the plane go up and down.

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Quick Navigation to Elevators

The Basics

  • 1. Definition and Explanation
  • 2. Main Functions
  • 3. Structure and Components

Operations

  • 4. How It Works
  • 5. Mechanisms and Their Functions
  • 6. Aerodynamics and Dynamics

A Closer Inspection

  • 7. Types of Elevators
  • 8. Using Trim
  • 9. Advancements and Innovations
  • 10. Watch Our “Elevators Explained” Video!

Functionality

  • 11. Controls and Forces
  • 12. Designs, Composition, and Trends

Pilot Mastery

  • 13. Flight Training and Simulators
  • 14. Incidents and Accidents

Purpose and Definition of an Elevator

How does an elevator work? Like many other airplane parts, it functions interactively. Located on the horizontal stabilizer of the tail section, the elevator adjusts the nose’s angle relative to the longitudinal axis. The elevator ensures flight stability and maneuverability making it essential to airplanes.

When I explain it to our aircraft mechanic students, I tell them it acts like a seesaw at the back of the plane, tilting the nose up or down as needed.

Do you ever wonder how a pilot knows exactly when to tilt the nose for landing? The elevator makes it happen! An elevator is a flight control surface that manages the aircraft’s pitch angle, which affects the flight path and altitude control. Its primary purpose is to help the pilot to safely fly the aircraft through climbing, cruising, and descending.

Main Functions of an Elevator

  • Pitch Control: First of all, the elevator adjusts the aircraft’s nose up or down for changes in altitude. Pitch control refers to the ability to control the up-and-down movement of the nose.
  • Stability: The elevator also provides balance when a plane experiences turbulence or shifts in weight distribution. Stability refers to a plane’s natural tendency to return to its normal flight condition after encountering turbulence or other disturbances.
  • Stall Prevention: Additionally, the elevator keeps the angle of attack within safe limits to avoid aerodynamic stalls. Stall prevention refers to a pilot’s actions to avoid an aerodynamic stall during flight.
  • Flight Path Management: Lastly, the elevator allows pilots to achieve precise adjustments for takeoff, cruising, and landing phases. Flight Path Management (FPM) refers to planning, executing, and monitoring a flight.

Structure and Location of the Elevator

You’ll find the elevator at the rear of the aircraft. It is an integral part of the empennage, or tail. This includes the horizontal stabilizer and vertical tailplane. Working together, these components take care of directional and pitch stability. At Epic, you’ll notice the empennage on all the planes in our fleet is painted bright red for visibility/safety.

Main Components of an Elevator

  • Horizontal Stabilizer: Also known as a tailplane, this is a fixed surface in the tail section of aircraft. It runs horizontal, hence its name, and provides balance and prevents the nose from bobbing up and down.
  • Elevator Trim Tabs: These are small, adjustable surfaces attached to the elevator so pilots can precisely adjust pitch trim.
  • Hinges: The hinges connect to the vertical stabilizer and allow the elevator to move.
  • Mechanical Systems: These include cables, pulleys, or advanced fly-by-wire systems that connect the elevator to the flight controls.

How the Elevator Works

The elevator operates by changing the angle of attack of the horizontal stabilizer (tailplane). This directly influences the aircraft’s lift and balance. Through this action, the elevator controls the position of the nose of the aircraft and the angle of attack of the wing.

Mechanisms and Their Functions

Pilots control the elevator using a yoke or control column connected to mechanical cables or fly-by-wire systems. They make precise adjustments during flight to maintain the flight path.

  • Upward Deflection: This produces downward lift at the tail, which raises the nose for the plane to climb.
  • Downward Deflection: This creates upward lift at the tail, which lowers the plane’s nose for descent.
  • Trim Adjustments: Pilots use trim to fine-tune the elevator position for stable cruising. This nuanced action makes the ride smoother.
  • Cable and Pulley Systems: These ensure mechanical reliability in conventional aircraft.
  • Hydraulic Assist: These are found in big jets and provide smoother and more consistent control forces.

Aerodynamics and Dynamics

The elevator is designed to follow basic aerodynamic principles. This enables it to adjust lift forces and stabilize the aircraft. By adjusting the airflow over the horizontal stabilizer, the elevator impacts pitch and overall flight dynamics. The same forces of flight that impact the aircraft also act on the elevator:

  • Lift: The wings generate lift, which is adjusted by elevator movements. Lift forces are directly altered by changes in the tailplane’s angle.
  • Weight: Weight is counteracted by lift, which creates balanced flight. Weight distribution is critical to prevent overcompensation. Whether carrying cargo or people, every pound matters.
  • Thrust: The power of thrust propels an aircraft forward, which allows pitch changes to change altitude.
  • Drag: The design of the elevator helps to minimize drag. The forces of thrust and drag are balanced to maintain efficient flight paths.

Why Dynamics Matter

Dynamic forces, including upward and downward deflection, have to be balanced so the aircraft stays within its flight envelope (range of operations). A pilot seeks this balance to ensure stability and prevent overcorrection during turbulence or high-speed maneuvers.

Types of Aircraft Elevators

There are different types of elevators, each of which is designed to meet specific aircraft requirements and design plans. These include:

  • Conventional Elevators: Like those found on Epic’s Cessna Skyhawks, these hinged movable surfaces are attached to the trailing edge of the horizontal stabilizer.
  • All-Moving Tailplanes (Stabilators): On this elevator, the entire horizontal stabilizer moves. These are commonly found in high-speed jets and transonic and supersonic aircraft.
  • Canard Elevators: These are placed at the aircraft’s front to enhance maneuverability in advanced configurations. Fun fact: The earliest canard was the Wright Flyer prototype.
  • T-Tail Elevators: Mounted on top of the vertical tailplane, these provide stability in larger aircraft.
  • Elevons: Used in delta-wing aircraft, this specialty elevator combines ailerons and elevator functionality. The Concorde is one example of a plane with an elevon.
  • Three-Surface Designs: Some aircraft, such as the Grumman X-29, include both forward (canard) and rear elevators for exceptional stability and control.
  • Slab: A “slab” refers to a type of horizontal stabilizer where the entire surface acts as an elevator.

Elevator Trim and Fine-Tuning: Finesse in Flight

The elevator trim system reduces a pilot’s workload by enabling small adjustments that maintain a steady pitch angle. This system uses trim tabs, small adjustable surfaces on the elevator, to ensure flight stability. Benefits of elevator trim include:

  • Reduction of pilot fatigue, especially during long-haul flights
  • Better fuel efficiency by maintaining optimal weight balance
  • Providing smoother altitude changes and stability

“When we work on elevators, we often need to manually deflect them up and down, sometimes while someone is sitting in the cockpit moving the controls. This is to check for proper movement, balance, and hydraulic response. Also, some elevators have counterweights to prevent aerodynamic flutter at high speeds. If we remove these weights during maintenance, the elevator can feel surprisingly light and even difficult to control until reinstalled.” –Josh Rawlins, Chief Operating Officer and Aircraft Mechanic Program Director

Advancements in Aircraft Elevators

The trim systems in modern aircraft dynamically adjust the elevator’s position for maximum efficiency and safety. Also, advanced diagram-based control interfaces in cockpits provide pilots with more intuitive ways to manage trim settings.

Modern elevators integrate cutting-edge technologies to improve performance, reliability, and safety. More recently, fly-by-wire systems have replaced traditional mechanical cables. This has led to increased precision.

Innovations in Elevator Systems

Designers are using active, or smart, materials capable of adjusting stiffness dynamically. They also focus on integrated aerodynamic features to improve airflow management. This reduces drag and increases efficiency.

  • Real-Time Diagnostics: This is a major win so pilots can monitor elevator performance to prevent potential failures.
  • Active Control Surfaces: Pilots love this aspect because elevators automatically adapt to changing flight conditions. This improves stability.
  • Enhanced Materials: Designers are using new smart composites to reduce weight and increase durability. Each of these innovations contribute to better maneuverability, fuel efficiency, and safety.
  • Diagrams: These help pilots visualize elevator functionality. They are critical for understanding the elevator’s role and highlight:
    • the interaction between elevator, horizontal stabilizer, and other flight controls.
    • the effects of upward/downward deflection on the flight path.
    • how aerodynamic forces affect pitch adjustments.

Aircraft Elevators Explained: Watch Our 7-Minute Video

How Do Elevators Interact with Secondary Flight Controls?

An elevator operates in harmony with other secondary flight controls, which ensures robust maneuverability and stability. For example:

  • Rudder: Controls yaw, which is the side-to-side motion about the vertical axis.
  • Ailerons: Manage roll, or the tilting motion around the longitudinal axis.
  • Flaps: Essential to enhance lift during takeoff and landing.

What is Coordinated Control?

Just as the name suggests, the pilot coordinates efficient interaction between the elevator, rudder, and ailerons to ensure seamless transitions between flight phases and precise control during maneuvers. These are critical during complex operations, such as a crosswind landings.

Challenges in Dynamic Forces

High-speed conditions and/or turbulence can increase dynamic forces on the elevator. Modern aircraft include feedback systems to help pilots effectively manage these conditions.

Elevator Designs: Considerations for Safety and Performance

Designers use careful planning to meet stringent safety and performance standards for elevators. Key considerations include:

  • Material Selection: Manufacturers should use high-strength yet lightweight materials for durability.
  • Failure Redundancy: Airplane safety often relies on backup systems to prevent catastrophic outcomes. When one feature fails, the backup system can make a world of difference.
  • Aerodynamic Efficiency: An optimized camber and chord line enable precise lift adjustments. Smooth and steady!

Composition

Aircraft manufacturers construct elevators today from durable, lightweight materials like carbon fiber composites and aluminum alloys. These materials reduce weight yet ensure structural integrity. Larger carriers typically use advanced materials to guarantee durability and efficient performance under heavy loads.

What Does the Future Hold in Elevator Design?

Manufacturers tell us that designers are working to integrate advanced materials and automation for improved performance and increased safety from the flight deck. Some of the trends we’ve been hearing about include these exciting ideas:

  • Flexible Wing Surfaces: They hope to replace separate control surfaces with adaptable materials. This could be a real game-changer.
  • Integrated Systems: Designers are planning to combine elevator functions with ailerons for streamlined control. Pilots are going to love that!
  • Automation: By leveraging AI-driven adjustments, designers believe they can reduce pilot workload and enhance safety. We are keeping an eye on all of this for our flight students as well as our aircraft mechanic students who will need to be trained on this new tech.

Pilot Training and Using the Elevator

Mastering elevator operation is a critical aspect of pilot training. Pilots must learn to coordinate pitch control with other systems for smooth flight and safe navigation. Since an aircraft moves in three dimensions, it operates along three distinct axes, each managed by specific flight controls. The aircraft pitches around its lateral axis using the elevator and rolls around its longitudinal axis using the ailerons.

Key training areas at Epic include:

  • Trim Adjustment: Using elevator trim to reduce manual input during extended flights.
  • Stall Prevention: Recognizing and recovering from dangerous flight conditions.
  • Altitude Management: Maintaining steady levels during turbulence or emergencies.

Can Pilots Learn to Operate Aircraft Elevators in a Simulator?

Absolutely! We rely on flight simulators at Epic so our pilots can practice all types of maneuvers safely. Simulators provide hands-on experience for pilots to perfect the management of the elevator under all types of scenarios. Pilots can replicate extreme conditions in aviation training devices (ATD) making them an important tool in effective flight training.

Incidents and Accidents Involving Elevators

In class, we often share historical events to emphasize a concept. Both pilots and aircraft mechanics learn about the causes of aviation tragedies in the hope to avoid history repeating itself. Epic’s motto is “Safety first!”

Below I’ve shared three deadly incidents involving the aircraft elevator.

1. Alaska Airlines Flight 261 ()

  • Incident: This tragic flight involved a McDonnell Douglas MD-83 that experienced a catastrophic failure of its horizontal stabilizer trim system, which directly affected the elevator’s functionality.
  • Key Role of Elevator: The jackscrew, which controlled the position of the horizontal stabilizer, failed due to inadequate lubrication over time. Focus for A&P mechanics? The importance of routine lubrication. Without proper stabilizer control, the pilots struggled to maintain pitch control using only the elevators. They managed to regain some control temporarily by inverting the aircraft, but the situation worsened, and the plane ultimately crashed.
  • Outcome: The investigation by the NTSB highlighted maintenance lapses and led to stricter regulations regarding inspections and lubrication of critical flight control components.

2. United Airlines Flight 232 ()

  • Incident: A McDonnell Douglas DC-10 experienced engine failure that caused severed hydraulic lines. This disabled all conventional flight controls, including the elevators.
  • Key Role of Elevator: With no hydraulic control over the elevator, rudder, or ailerons, the crew was forced to use differential engine thrust to control pitch, roll, and yaw. Despite having no functional elevators, the pilots managed to reach Sioux City, Iowa for an attempted emergency landing.
  • Outcome: The crash resulted in fatalities, however, 185 out of 296 passengers did survive. This flight became a landmark case in human ingenuity and teamwork under extreme conditions. It also emphasized the importance of redundancy in flight control systems.

3. Japan Airlines Flight 123 ()

  • Incident: A Boeing 747SR experienced a rapid decompression due to a faulty rear pressure bulkhead repair. The decompression damaged the rear vertical and horizontal stabilizers. This severely impaired the elevators.
  • Key Role of Elevator: With damaged elevators and limited stabilizer effectiveness, the pilots could not control the aircraft’s pitch and descent rate. The flight ultimately crashed into a mountainside. Today, this incident remains a stark example of how critical the empennage (tail section) is to aircraft stability and control.
  • Outcome: This was one of the deadliest single-aircraft accidents in history. It led to more robust scrutiny of maintenance practices and repair quality, a point we drive home in our classes.

Onward and Upward

I have worked on countless elevators myself as an A&P mechanic, and I can assure you the elevator is an indispensable part of an aircraft’s control system. The elevator ensures precise pitch control, safe altitude management, and overall flight stability.

Ongoing development in design, materials, and technology underscore its importance in the aviation world. As aircraft evolve, so will their control surfaces, making elevators more sophisticated, reliable, and efficient. Whether you’re piloting or maintaining an aircraft, understanding the elevator’s role is key to safety.

Join the Forum Discussion on Elevator in an Aircraft Below!

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About the Author

Josh Rawlins

Josh Rawlins, a native of New Smyrna Beach, grew up just a few miles from Epic Flight Academy. At age 19, he began working at Epic, sweeping hangar floors and assisting coworkers with various tasks. What started as a humble job quickly evolved into a lifelong career in aviation.

Over time, Josh demonstrated remarkable initiative. While working at Epic, he completed accounting courses, earned his A&P mechanic license, and obtained inspection authorization. These achievements propelled him to Lead Mechanic and, later, Director of Maintenance.

  • Josh's dedication to safety, hard work, and commitment to Epic earned him the title of Vice President and, in , Chief Operating Officer and board member. In , he also took on the role Aircraft Mechanic Program Director.
  • Josh has earned significant recognition for his contributions to aviation. In , the National Business Aviation Association honored him with the Business Aviation Top 40 Under 40 Award in Maintenance. He was also named a "Top 40 Under 40" honoree by the Daytona News-Journal in .

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How Airplane Lift Works - Pilot Institute

On a windy December morning in , two brothers from Dayton, Ohio, made history. In just 12 seconds, the dream of powered human flight became a reality.

Aeronautical science has advanced dramatically since the Wright brothers’ flight at Kitty Hawk. It’s tempting to assume we’ve solved the mysteries of flight.

But did you know that scientists still debate how a wing creates lift? There is yet to be a singular explanation for the force that keeps airplanes aloft.

In this article, we’ll explore how early aviators discovered the magic of lift. We’ll also find out why, despite decades of research, engineers still can’t agree on how wings do what they do.

Key Takeaways

  • Bernoulli’s theorem describes how pressure differences on a wing create lift.
  • Newton’s laws of motion describe how the downward deflection of air creates an upward lift force.
  • Neither Newton’s laws nor Bernoulli’s theorem entirely explain how wings generate lift.

Inventing the Wing

You might wonder how the airplane wing came about, considering we don’t fully know how lift works.

Well, the short answer is that we copied the blueprint from nature.

In the early 19th century, British inventor Sir George Cayley translated the shape of a bird’s wing into the modern airfoil. An airfoil is a shape designed to create lift.

Cayley’s studies led him to discover the importance of camber. Camber is the curvature of a wing. Airfoils with a larger curve on top than the bottom have a positive camber. Symmetrical airfoils have the same curve above and below the chord line. The chord line is an imaginary line from the wing’s leading edge to its trailing edge.

Airfoil Camber

Cayley discovered that a wing with a positive camber created more lift than a symmetrical or flat wing. Cambered wings were also more resistant to stalling.

His investigations didn’t stop there. Cayley pinpointed the four forces of flight: lift, weight, thrust, and drag. He also wrote extensively on aircraft control and stability. Amazingly, Cayley did this about 100 years before the Wrights’ first powered flight. 

Many of Cayley’s insights hold up surprisingly well. In his paper “On Aerial Navigation,” he suggested that the upper camber “creates a slight vacuity.” In other words, the curved top of the wing creates a partial vacuum when air passes over it. This more than hints at one of the scientific theories of lift we’ll discuss later.

The Origins of Modern Aeronautics

The invention of the wind tunnel by Frank Wenham in was a turning point in our understanding of the physics of lift. A wind tunnel is a device that allows engineers to test an airfoil’s lift, drag, and pressure distribution. Finally, inventors could consistently test their wing designs.

The Wrights would put Wenham’s invention to good use 30 years later.

The Wind Tunnel: A Controlled Environment

During the - flying season, the Wright brothers struggled with their glider design. Their wing provided less lift than data from their late friend Otto Lilienthal said it would. 

So, in the autumn of , the Wrights built the second wind tunnel in the United States. Their wind tunnel was the key to their successful airfoils. And they didn’t even have to leave their bicycle shop to use it.

The Pressure Connection

George Cayley knew back in that air pressure was lower on the top of an airfoil than on the bottom.

The Wrights clearly understood the association between accelerated airflow on the top of the wing and lower pressure. They knew that the pressure difference between the top and bottom of the wing creates lift. But the Wrights never published any theories on why this might be.

For more information, please visit aviation lifts.

It turns out the explanation would come from an 18th-century Swiss mathematician.

Bernoulli’s Theorem

George Cayley and the Wright brothers never mentioned Daniel Bernoulli by name in their writings, but they indirectly echoed his discoveries.  

Bernoulli was born in into a family of mathematicians. Unsurprisingly, he became a mathematician as well. 

But at his father’s request, he also studied medicine. His exploration of blood pressure gave him insight into the physical properties of fluids.

Hydrodynamica

In his work Hydrodynamica, Bernoulli used the principle of conservation of energy to describe fluid dynamics.

Bernoulli’s theorem states that when the velocity of a fluid increases, the static pressure decreases, and vice versa. This relationship applies to any fluid in a streamline: liquid or gas.

Bernoulli never applied his theorem to the creation of lift in his lifetime. However, it explains what we see with airflow over a wing. 

The air on top of the wing moves faster, corresponding with an area of low pressure. The higher pressure under the wing pushes up toward the lower pressure over the wing. This pressure differential is the lift force.

Bernoulli’s theorem became a popular way to explain lift in the following decades. However, it fails to explain why the top of the wing accelerates the air in the first place. This confusion drove many incorrect explanations over the years.

Incorrect Applications of Bernoulli

One common misunderstanding of Bernoulli’s principle is the “equal transit-time” theory. 

The explanation goes something like this. 

When a parcel of air hits the airfoil’s leading edge, it “splits” in two. The curved top of the airfoil creates a longer path for air molecules to travel than the bottom. So, for the air molecules on the top to meet up with air molecules on the bottom at the trailing edge, they must go faster. This increase in velocity causes a decrease in pressure, creating lift.

While this argument is tempting, it doesn’t stand up to scrutiny.

First, there is no reason why the air on top must simultaneously meet back up with the air on the bottom. The molecules are not “bound” to each other in any way.

Second, the air on top accelerates to a faster speed than this explanation requires. A parcel of air above the wing reaches the trailing edge before its below-wing equivalent.

As it turns out, a cambered wing is not required for lift production. Symmetrical airfoils work just fine. 

Stranger still, even a flat plate generates lift.

Flying the Barn Door

There’s an old saying in aviation that goes, “with a big enough engine, you can fly a barn door.”

And as silly as it sounds, there’s some truth to that. As un-aerodynamic as a barn door is, it can produce lift.

But how?

One key aspect of lift generation is the wing’s angle of attack. The angle of attack is the angle between the chord line of the wing and the relative wind. The relative wind is the direction the wing “feels’ the air is coming from. For an airplane, the relative wind is always opposite the direction of travel.

As the angle of attack increases, the pressure difference between the top and bottom of the wing increases. This differential causes lift to increase. Up to a point, anyway.

Once the wing reaches the critical angle of attack, any further increase in angle causes the airflow to separate from the wing’s surface. At this point, the wing stalls, and lift is significantly reduced.

A flat-plate wing creates extremely turbulent airflow at a higher angle of attack. The wing stalls quickly. But at a very low angle of attack, a flat wing works much like an airfoil, just not very efficiently. (A smooth shape resists stalling.) Airflow splits in two, and the top side has a lower pressure than the bottom, creating lift.

If that’s hard to believe, try it for yourself using NASA’s interactive airfoil simulation.

Similarly, a symmetrical airfoil works just fine to create lift. At zero angle of attack, the top and bottom pressures are equal, so there is no lift. But when the angle of attack increases, we see similar pressure patterns as with positively cambered airfoils.

Symmetrical airfoils are perfect for aerobatic airplanes that frequently fly inverted. But cambered airfoils can fly upside down as well. This feat simply requires a higher angle of attack.

So, not only is camber unnecessary to generate lift, but its lift-enhancing effects can be “overpowered” by angle of attack.

If lift doesn’t require a curved airfoil, how do we explain what creates the low pressure on top of a wing?

Enter Newton.

Newton’s Laws of Motion

Isaac Newton’s masterwork Principia took the scientific world by storm. For the first time,  science could mathematically explain the physical motion of bodies. 

Newton’s second law of motion states that any time a mass is accelerated, it imposes a net force. By acceleration, we mean a change in the speed or direction of the mass.

Although we don’t often think of air as particularly “heavy,” it has mass. When an airfoil slices through the air, its shape and angle of attack cause the airflow to accelerate and deflect downward. This “downwash” follows the airfoil’s contour, imparting a downward force.

And here’s where Newton’s third law comes in. This law states that for every action, there is an equal and opposite reaction. That is the conservation of momentum. So, when the airfoil accelerates the air downwards, an equal and opposite force accelerates the airfoil upwards.

This upward force is another way to explain lift.

Newton’s laws are not in opposition to Bernoulli’s theorem. They both describe the same lift force through different means. In fact, you can derive Bernoulli’s theorem directly from Newton’s second law.

Describing Lift is not Explaining Lift

You may have guessed that this is where the explanation of lift takes a complicated turn. Neither Bernoulli’s theorem nor Newton’s laws explain why an airfoil creates lift in the first place. And neither directly explains why the airfoil turns the air downward. They only describe the manifestations of lift.

We can think of lift as a relationship between four elements: an increase in airflow speed over the wing, a decrease in pressure over the wing, an increase in pressure under the wing, and a downward turning of the airflow. 

The missing piece of the puzzle is what ties these elements together. 

How do we create a complete theory of lift? Unfortunately, there is no easy solution to this predicament.

A Unified Theory of Lift?

Do you plan on diving deeper into the origins of lift? Be ready to come face-to-face with several complicated theories and models. 

There are pressure and velocity fields around the airfoil to consider. Don’t forget the Navier-Stokes equations. And then there’s the impact of viscosity to study. 

The Coandă effect seems promising to explain why air follows the airfoil’s curve. However, its direct application to the explanation of lift is controversial.

The Kutta-Joukowski theorem describes circulatory airflow around an airfoil. It’s a common explanation for how lift starts on a wing. However, it only mathematically expresses the circulation. It doesn’t provide a physical cause.

Even in , scientists are still working on new theories of lift. But one singular, clear explanation of lift has yet to satisfy all the requirements.

We may be waiting quite a while for a Unified Theory of Lift.

Conclusion

Aeronautical science has come a long way since those primitive years of wooden wind tunnels and hand-plotted graphs.

Today, we can design aircraft with a level of precision early aviators only dreamed of. Modern aircraft are faster, more efficient, and safer than ever before. But even with our sophisticated computer models, we still cannot provide a universal explanation for lift.

Are you interested in learning more about tree care landscaping lifts? Contact us today to secure an expert consultation!

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