Pilot Institute

NOVEMBER 11, 2024

How an aircraft handles Dutch roll depends on its dynamic stability. The aircraft’s design influences its dynamic stability. Increased lift on the raised wing immediately creates more induced drag. What’s induced drag? The higher drag on the raised wing reduces its speed relative to the lower wing.

Stability 52

Stability Center of Gravity Aileron Rudder 52

Pilot's Life Blog

MARCH 15, 2024

Below are other critical pieces of the wings that help give the plane additional lift, reduce drag, or achieve lower speeds in preparation for landing: Ailerons: A French word meaning “fin” or “little wing,” the aileron helps control the airplane’s roll. What are the basic parts of this section?

Horizontal Stabilizer 52

Horizontal Stabilizer Aileron Air Traffic Control Lift 52

Northstar VFR

JULY 21, 2024

The rudder is a movable flight control which is mounted on the trailing edge of the vertical stabilizer on the back of the airplane. Some new student pilots think the rudder and vertical stabilizer are the same thing. The vertical stabilizer is a vertical fixed part of the plane’s empennage. Why is the rudder so important?

Rudder 52

Rudder Airplanes Pilot Stability 52

Vintage Aviation News

JULY 23, 2024

This is consistent with the theory, as a displaced torpedo would have bulged the bomb bay doors, which wind resistance could then have pealed back – leading to a rapid increase in drag preventing the aircraft from gaining altitude at sufficient speed.

Cockpit 130

Cockpit Runway Drag Pilot 130

Vintage Aviation News

OCTOBER 11, 2024

However, this wasn’t the only unique thing about Cierva Twin; it was outstanding in its class for the following reasons – Coaxial Rotor System – This design eliminated the need for a tail rotor, reducing mechanical complexity and increasing lift efficiency. This allowed for more stability and control, especially in hover.

Tail 52

Tail Drag Ceiling Cargo 52

Pilot Institute

FEBRUARY 20, 2025

What Is Aircraft Stability? Stability is the aircrafts tendency to maintain its attitude or orientation. This means that they have to be effective enough to counter the aircrafts inherent lateral stability. Lateral stability depends on the aircrafts design. potentially reverting the aileron back into a tail-heavy state.

Aileron 90

Aileron Weight-Shift-Control Rudder Longitudinal Axis 90

Airspeed Junkie

AUGUST 2, 2024

Notable design changes included the introduction of a swept tail design in 1960 and a new cowl design in 1961, which improved aerodynamics and performance. With a maximum takeoff weight of 2,400 pounds and a maximum gross weight that ensures stability, this aircraft is robust enough to handle a variety of flying conditions.

Knot 98

Knot Cockpit Pilot Gross Weight 98

Pilot Institute

NOVEMBER 1, 2024

And ice doesn’t just make things slippery, it messes with the airflow over the wings, cuts down on lift, and ramps up drag. Remember that wings, propeller blades, and tail surfaces are airfoil-shaped. This leads to a serious loss of lift and an increase in drag. If you don’t act quickly, you’ll soon feel its effects.

Pitot Tube 52

Pitot Tube Drag Lift Airfoil 52

Fear of Landing

MARCH 22, 2024

Gradually used to replace metals on parts of aircraft tails, wings, engines, cowlings, and parts of the fuselage, composites reduce overall aircraft weight and improve operational efficiency. Area Rule In the 1950s, NASA scientist Richard Whitcomb discovered several fundamental solutions to key aerodynamics challenges.

Wind Shear 52

Wind Shear Airfoil Drag Airlines 52

Aerotime

MARCH 27, 2025

Following D-Day, as the war began to tail off, Yeager returned to fly combat missions, as Eisenhower yielded to Yaeger’s demands. Through their research, engineers at Bell Aircraft discovered that bullets could maintain stability at supersonic speeds due to their shape, leading them to design the fuselage of the X-1 along similar lines.

Pilot 275

Pilot Drag Airplanes Stability 275

Pilot Institute

MARCH 26, 2024

However, the increased drag might make it impossible to take off again. As with any landing, it’s vital to have a stabilized approach. If you’re not stabilized at 200 feet AGL, go around. Make sure not to pull back too hard, or you could cause a tail strike. A field with tall grass will slow you down quickly on landing.

NOTAMs 52

NOTAMs Runway Approach Descent 52

Vintage Aviation News

DECEMBER 14, 2024

It was certainly a most unusual aircraft, distinguished by its forward swept wing and canard horizontal stabilizers. This was why the strakes were added to the X-29’s tail, in order to reduce drag from using the trim on the canard in the nose.

Horizontal Stabilizer 96

Horizontal Stabilizer Center of Gravity Tail Drag 96

Pilot Institute

FEBRUARY 15, 2025

At first, you might experience a strong headwind, which briefly increases your airspeed and gives you a false sense of stability. A massive explosion followed, and the tail section skidded backward. Keep wings level to prevent unnecessary drag or instability. Within seconds, everything changes. Dont lower the nose!

Wind Shear 66

Wind Shear Weather Descent Approach 66

Vintage Aviation News

OCTOBER 22, 2024

Additionally, the design featured a large engine, small wings with high wind loading, and a focus on low-altitude stability. The aircraft felt underpowered and, faced issues with transonic drag, and went under further refinements in the design. Such emphasis was of major importance for delivering nuclear bombs. Jack” D.T.W.

Weather 97

Weather Drag Payload Stability 97

Plane and Pilot

OCTOBER 3, 2024

True, a slightly higher aspect ratio wing was desired, which in turn required a larger vertical tail and thus a little extra mass, but the size, approximately 20% larger than a Widgeon, was set. The airfoil is a Harry Riblett shape, giving modernized flow separation on the leading edge for a soft stall yet with good lift and drag performance.

Airplanes 80

Airplanes Rudder Knot Aileron 80

Plane and Pilot

DECEMBER 16, 2024

Planespotters note the F2’s separate ailerons and flaps, conventional tail. Out back, theres an entirely new tail. The previous CTs had a stabilator for pitch, where the new F2 uses a more conventional elevator and fixed horizontal stabilizer.

Airplanes 98

Airplanes Rudder Aileron Crosswind 98