An analytical trend study of propeller whirl instability /

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

Flight investigation of effects of selected operatings conditions on the bending and torsional moments encountered by a helicopter rotor blade /

Ludi, LeRoy H.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Transonic flutter tests of a highly swept arrow wing with and without simulated trailing-edge-mounted engine masses /

Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Stresses and loads.Includes bibliographical references.Mode of access: Inte...

Some recent studies in structural dynamics of rotor aircraft /

Brooks, George W.
Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

An investigation of periodic forces and moments transmitted to the hub of the four lifting rotor configurations /

Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Propulsion systems, air-jet; Stresses and loads.Includes bibliographical re...

Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees /

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bi...

Transonic and supersonic flutter trend investigation of a variable-sweep wing /

Stonesifer, John C.
Goetz, Robert C.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

The effect of blade flapping on the dynamic stability of a tilting-rotor convertiplane /

Quigley, Hervey C.
Koenig, David G.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical refe...

Shock-wave patterns on a cranked-wing configuration /

Sammonds, Robert I.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles.Includ...

Calculated mode shapes and pressure distributions at flutter for a highly tapered horizontal tail in subsonic flow /

Hunt, Gerald L.
Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Study of flow over oscillating airfoil models at a mach number of 7.0 in helium /

Arman, Ali
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Stresses and loads.Includes bibliographical references.Mode of access: I...

An analysis of the flapwise bending frequencies and mode shapes of rotor blades having two flapping hinges to reduce vibration levels /

Brooks, George W.
Leonard, H. Wayne.
United States. National Aeronautics and Space Administration.

Cover title."December 1960."Aircraft; Stresses and loads.Includes bibliographical references.Mode of...

An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds

Whitcomb, Charles F.
Critzos, Chris C.
Brown, Philippa F.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loa...

Structural-loads surveys on two tilt-wing VTOL configurations /

Ward, John F.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode of ac...

Review of propeller-rotor whirl flutter /

Reed, Wilmer H., III.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

Work performed at Langley Research Center."July 1967."Includes bibliographical references (p. 26-27)...

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

Flight investigation of effects of selected operatings conditions on the bending and torsional moments encountered by a helicopter rotor blade /

Ludi, LeRoy H.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Transonic flutter tests of a highly swept arrow wing with and without simulated trailing-edge-mounted engine masses /

Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Stresses and loads.Includes bibliographical references.Mode of access: Inte...

Some recent studies in structural dynamics of rotor aircraft /

Brooks, George W.
Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

An investigation of periodic forces and moments transmitted to the hub of the four lifting rotor configurations /

Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Propulsion systems, air-jet; Stresses and loads.Includes bibliographical re...

Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees /

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bi...

Transonic and supersonic flutter trend investigation of a variable-sweep wing /

Stonesifer, John C.
Goetz, Robert C.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

The effect of blade flapping on the dynamic stability of a tilting-rotor convertiplane /

Quigley, Hervey C.
Koenig, David G.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical refe...

Shock-wave patterns on a cranked-wing configuration /

Sammonds, Robert I.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles.Includ...

Calculated mode shapes and pressure distributions at flutter for a highly tapered horizontal tail in subsonic flow /

Hunt, Gerald L.
Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Study of flow over oscillating airfoil models at a mach number of 7.0 in helium /

Arman, Ali
United States. National Aeronautics and Space Administration.

Cover title."December 1961."Stresses and loads.Includes bibliographical references.Mode of access: I...

An analysis of the flapwise bending frequencies and mode shapes of rotor blades having two flapping hinges to reduce vibration levels /

Brooks, George W.
Leonard, H. Wayne.
United States. National Aeronautics and Space Administration.

Cover title."December 1960."Aircraft; Stresses and loads.Includes bibliographical references.Mode of...

An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds

Whitcomb, Charles F.
Critzos, Chris C.
Brown, Philippa F.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loa...

Structural-loads surveys on two tilt-wing VTOL configurations /

Ward, John F.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode of ac...

Review of propeller-rotor whirl flutter /

Reed, Wilmer H., III.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

Work performed at Langley Research Center."July 1967."Includes bibliographical references (p. 26-27)...

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

Flight investigation of effects of selected operatings conditions on the bending and torsional moments encountered by a helicopter rotor blade /

Ludi, LeRoy H.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Transonic flutter tests of a highly swept arrow wing with and without simulated trailing-edge-mounted engine masses /

Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Stresses and loads.Includes bibliographical references.Mode of access: Inte...

An analytical trend study of propeller whirl instability /

Abstract

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An analytical trend study of propeller whirl instability /

Abstract

Extracted data

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