Explore Books on
stalling (aerodynamics)
1-24 of 61 Books
Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft
Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft
By E. Richard White
In-flight loss of control, leading to forced landing and runway overrun, Continental Express, Inc., N24706, Embraer EMB-120 RT, Pine Bluff, Arkansas, April 29, 1993
In-flight loss of control, leading to forced landing and runway overrun, Continental Express, Inc., N24706, Embraer EMB-120 RT, Pine Bluff, Arkansas, April 29, 1993
By United States. National Transportation Safety Board.
Rotary balance data for a single-engine trainer design for an angle-of-attack range of 8 ̊to 90/̊
Rotary balance data for a single-engine trainer design for an angle-of-attack range of 8 ̊to 90/̊
By Paul Pantason
Analysis of strong-interaction dynamic stall for laminar flow on airfoils
Analysis of strong-interaction dynamic stall for laminar flow on airfoils
By H. J. Gibeling
Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes
Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes
By Dale R. Satran
A theory of rotating stall of multistage axial compressors
A theory of rotating stall of multistage axial compressors
By F. K. Moore
Water-tunnel experiments on an oscillating airfoil at RE = 21,000
Water-tunnel experiments on an oscillating airfoil at RE = 21,000
By Kenneth W. McAlister
Simulation study of the oscillatory longitudinal motion of an airplane at the stall
Simulation study of the oscillatory longitudinal motion of an airplane at the stall
By William H. Phillips
Aborted takeoff shortly after liftoff, Trans World Airlines flight 843, Lockheed L-1011, N11002, John F. Kennedy International Airport, Jamaica, New York, July 30, 1992
Aborted takeoff shortly after liftoff, Trans World Airlines flight 843, Lockheed L-1011, N11002, John F. Kennedy International Airport, Jamaica, New York, July 30, 1992
By United States. National Transportation Safety Board.
Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes
Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes
By Dale R Satran
Analysis of strong-interaction dynamic stall for laminar flow on airfoils
Analysis of strong-interaction dynamic stall for laminar flow on airfoils
By H. J Gibeling
Compressor instability with integral methods
By Y. K. Eddie Ng
Water-tunnel experiments on an oscillating airfoil at RE = 21,000
Water-tunnel experiments on an oscillating airfoil at RE = 21,000
By Kenneth W McAlister
A theory of post-stall transients in multistage axial compression systems
A theory of post-stall transients in multistage axial compression systems
By F. K. Moore
Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane
Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane
By H. Paul Stough
General aviation pilot stall awareness training syllabus
General aviation pilot stall awareness training syllabus
By United States Federal Aviation Administration
Effect of an extendable slat on the stall behavior of a VR-12 airfoil
Effect of an extendable slat on the stall behavior of a VR-12 airfoil
By
Aircraft stalling and buffeting
Aircraft stalling and buffeting
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Consultant and Exchange Programme.
Subsonic/transonic stall flutter investigation of a rotating rig
Subsonic/transonic stall flutter investigation of a rotating rig
By
A study of lightplane stall avoidance and suppression
A study of lightplane stall avoidance and suppression
By David R. Ellis
Subsonic/transonic stall flutter investigation of a rotating rig
Subsonic/transonic stall flutter investigation of a rotating rig
By
Comparison of dynamic stall phenomena for pitching and vertical translation motions
Comparison of dynamic stall phenomena for pitching and vertical translation motions
By T. Fukushima