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Explore Books on
stalling (aerodynamics)

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View 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

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

View A theory of rotating stall of multistage axial compressors By F. K. Moore

A theory of rotating stall of multistage axial compressors

A theory of rotating stall of multistage axial compressors

By F. K. Moore

View Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes By Dale R. Satran

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

View Analysis of strong-interaction dynamic stall for laminar flow on airfoils By H. J. Gibeling

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

View Rotary balance data for a single-engine trainer design for an angle-of-attack range of 8 ̊to 90/̊ By Paul Pantason

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

View 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.

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.

View Water-tunnel experiments on an oscillating airfoil at RE = 21,000 By Kenneth W. McAlister

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

View Anatomy of a Spin By John Lowery
Cover of Anatomy of a Spin by john lowery

Anatomy of a Spin

By John Lowery

View Stalls, spins, and safety By Sammy Mason
Cover of Stalls, spins, and safety by sammy mason

Stalls, spins, and safety

By Sammy Mason

View A theory of post-stall transients in multistage axial compression systems By F. K. Moore

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

View Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes By Dale R Satran

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

View Compressor instability with integral methods By Y. K. Eddie Ng
Cover of Compressor instability with integral methods by y. k. eddie ng

Compressor instability with integral methods

By Y. K. Eddie Ng

View 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.

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.

View Simulation study of the oscillatory longitudinal motion of an airplane at the stall By William H. Phillips

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

View Analysis of strong-interaction dynamic stall for laminar flow on airfoils By H. J Gibeling

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

View Water-tunnel experiments on an oscillating airfoil at RE = 21,000 By Kenneth W McAlister

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

View Low-speed wind-tunnel tests on the effects of tailplane and nacelle position on the superstall characteristics of transport aircraft By David John Kettle

Low-speed wind-tunnel tests on the effects of tailplane and nacelle position on the superstall characteristics of transport aircraft

Low-speed wind-tunnel tests on the effects of tailplane and nacelle position on the superstall characteristics of transport aircraft

By David John Kettle

View All about stalls & spins By Everett Gentry
Cover of All about stalls & spins by everett gentry

All about stalls & spins

By Everett Gentry

View Messung von instationären Drücken bei Stall und Buffeting By P. Bublitz

Messung von instationären Drücken bei Stall und Buffeting

Messung von instationären Drücken bei Stall und Buffeting

By P. Bublitz

View Half-speed bearing whirl excited by a single propagating stall cell in a multi-stage axial-flow compressor By John Ringrose

Half-speed bearing whirl excited by a single propagating stall cell in a multi-stage axial-flow compressor

Half-speed bearing whirl excited by a single propagating stall cell in a multi-stage axial-flow compressor

By John Ringrose

View Wind tunnel measurements of the low speed stalling characteristics of a model of the Hawker-Siddeley trident 1C By Donald Isaacs

Wind tunnel measurements of the low speed stalling characteristics of a model of the Hawker-Siddeley trident 1C

Wind tunnel measurements of the low speed stalling characteristics of a model of the Hawker-Siddeley trident 1C

By Donald Isaacs

View Airfoil interaction with an impinging vortex By Kenneth W. McAlister
Cover of Airfoil interaction with an impinging vortex by kenneth w. mcalister

Airfoil interaction with an impinging vortex

By Kenneth W. McAlister

View Flying beyond the stall By Douglas A. Joyce

Flying beyond the stall

Flying beyond the stall

By Douglas A. Joyce

View Uncontrolled flight into terrain, ABX Air (Airborne Express), Douglas DC-8-63, N827AX, Narrows, Virginia, December 22, 1996 By United States. National Transportation Safety Board.

Uncontrolled flight into terrain, ABX Air (Airborne Express), Douglas DC-8-63, N827AX, Narrows, Virginia, December 22, 1996

Uncontrolled flight into terrain, ABX Air (Airborne Express), Douglas DC-8-63, N827AX, Narrows, Virginia, December 22, 1996

By United States. National Transportation Safety Board.