Remove Airfoil Remove Airplanes Remove Stability
article thumbnail

Tailless Aircraft: How Airplanes Fly Without a Tail

Pilot Institute

Have you ever seen an airplane with no tail and no vertical fin, but with just a sleek wing? A tailless aircraft is a fixed-wing airplane without a horizontal stabilizing surface. With this type of aircraft, the functions of longitudinal stability and control are incorporated into the main wing. How does the tail do this?

Tail 52
article thumbnail

Mastering Stalls: How to Recognize, Prevent, and Recover Safely

Flight Training Central

Depending on design, airfoils used in general aviation, stall at angles of attack between 16 to 18 degrees. A wing will always stall at the same angle of attack; however, weight, and bank angle, power setting and load factor may change the speed or the pitch attitude at which the airplane stalls.

Rudder 96
Insiders

Sign Up for our Newsletter

This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.

Trending Sources

article thumbnail

Flight Test Files: Convair XF-92A Dart

Vintage Aviation News

The delta wing’s large area (425 square feet), thin airfoil cross section, low weight, and structural strength made a great combination for a supersonic aircraft. Photo NACA/NASA The single-place XF-92A airplane had a delta wing swept at 60 degrees. feet high at the tip of the vertical stabilizer. feet long, had a 31.3-foot

Airfoil 64
article thumbnail

Flight Test Files: B-47A Stratojet

Vintage Aviation News

In 1954 this photo of two swept wing airplanes was taken on the ramp of NACA High-Speed Flight Research Station. Langley was particularly focused on structural loads, while Ames concentrated on dynamic stability. The drag chute was used on landings to help brake the airplane’s speed.

article thumbnail

Learning Aeronautical Engineering From Historic Aircraft Designs

Vintage Aviation News

Studying historical aircraft helps students understand the development of flight and learn from early engineers about problems of lift, propulsion, stability, and material constraints. With the right support, future engineers can deepen their understanding of aviation history while developing the skills necessary for innovation.

Drag 52
article thumbnail

Flight Test Files: B-47A Stratojet

Vintage Aviation News

NACA laboratories had an interest in B-47A NACA 150; Langley Memorial Laboratory wished to study the impact of aeroelasticity upon structural loads and Ames Aeronautical Laboratory, the impact of aeroelasticity upon dynamic stability. Operation of the aircraft from either Center was not practical because of runway length. long and thin).

Airfoil 98
article thumbnail

Today in Aviation History: First Flight of the Stipa-Caproni

Vintage Aviation News

During these years, he concluded that the inner surface of the venturi tube needed an airfoil shape to achieve the greatest efficiency. The duct, as predicted by Stipa, had a profile similar to that of the airfoil, with a fairly small rudder and elevators mounted on the trailing edge of the duct. The Stipa-Caproni in flight.

Airfoil 98