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

Flight measurements of the effects of blade out of track on the vibration levels on a tandem rotor helicopter /

United States. National Aeronautics and Space Administration.
Langley Research Center.

"May 1960."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

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...

Characteristics at mach number of 2.03 of a series of wings having various spanwise distributions of thickness ration and chord /

Robins, A. Warner.
Jackson, Charlie M.
Harris, Roy V.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aircraft.Includes bibliographical references.Mode of access: Internet

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...

Theoretical investigation of the subsonic and supersonic flutter characteristics of a swept wing employing a tuned sting-mass flutter suppressor /

Yates, E. Carson.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Stresses and loads.Includes bibliographical references.Mode of access: I...

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...

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...

Dynamic-model of the damping of flapwise bending modes of two-blade rotors in hovering and a comparison with quasi-static and unsteady aerodynamic theories /

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

Cover title."December 1959."Wings rotating, experimental studies; Loads, rotating wings; Vibration a...

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...

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...

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...

Experimental determination of the pressure distribution on a rectangular wing oscillating in the first bending mode for mach numbers from 0.24 to 1.30 /

Lessing, Henry C.
Menees, Gene P.
Troutman, John L.
United States. National Aeronautics and Space Administration.

Cover title."December 1960."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical refe...

Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45 degree sweptback wing at transonic speeds /

Arabian, Donald D.
Reid, Charles F.
Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode o...

Fatigue investigation of full-scale transport-airplane wings tests with constant-amplitude and variable amplitude loading schedules/

Foster, Lee R.
Whlaey, Richard E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Stresses and loads.Includes bibliographical references.Mode of access: In...

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...

Flight measurements of the effects of blade out of track on the vibration levels on a tandem rotor helicopter /

United States. National Aeronautics and Space Administration.
Langley Research Center.

"May 1960."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

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...

Characteristics at mach number of 2.03 of a series of wings having various spanwise distributions of thickness ration and chord /

Robins, A. Warner.
Jackson, Charlie M.
Harris, Roy V.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aircraft.Includes bibliographical references.Mode of access: Internet

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...

Theoretical investigation of the subsonic and supersonic flutter characteristics of a swept wing employing a tuned sting-mass flutter suppressor /

Yates, E. Carson.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Stresses and loads.Includes bibliographical references.Mode of access: I...

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...

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...

Dynamic-model of the damping of flapwise bending modes of two-blade rotors in hovering and a comparison with quasi-static and unsteady aerodynamic theories /

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

Cover title."December 1959."Wings rotating, experimental studies; Loads, rotating wings; Vibration a...

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...

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...

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...

Experimental determination of the pressure distribution on a rectangular wing oscillating in the first bending mode for mach numbers from 0.24 to 1.30 /

Lessing, Henry C.
Menees, Gene P.
Troutman, John L.
United States. National Aeronautics and Space Administration.

Cover title."December 1960."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical refe...

Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45 degree sweptback wing at transonic speeds /

Arabian, Donald D.
Reid, Charles F.
Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode o...

Fatigue investigation of full-scale transport-airplane wings tests with constant-amplitude and variable amplitude loading schedules/

Foster, Lee R.
Whlaey, Richard E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Stresses and loads.Includes bibliographical references.Mode of access: In...

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...

Flight measurements of the effects of blade out of track on the vibration levels on a tandem rotor helicopter /

United States. National Aeronautics and Space Administration.
Langley Research Center.

"May 1960."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

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...

Characteristics at mach number of 2.03 of a series of wings having various spanwise distributions of thickness ration and chord /

Robins, A. Warner.
Jackson, Charlie M.
Harris, Roy V.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aircraft.Includes bibliographical references.Mode of access: Internet

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

Abstract

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

Abstract

Extracted data

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