Experimental investigation of oscillatory aerodynamic forces, moments and pressures acting on a tapered wing oscillating in pitch at mach numbers from 0.40 to 1.07 /

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...

Analytical and experimental investigation of flutter and divergence of speed-mounted cone configurations at supersonic speeds / y John L. Sewall, Robert W. Hess and Charles E. Watkins.

Sewall, John L.
Watkins, Charles E.
Hess, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Stresses and lo...

Velocity potential and forces on oscillating slender bodies of revolution in supersoni flow expanded to the fifth power of the frequency /

Lansing, Donald L.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

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...

An investigation of the influence of lift on sonic-boom intensity by means of wind-tunnel measurements of the pressure fields of several wing-body combinations at a mach number of 2.01 /

Carlson, Harry W.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircraft ...

Aerodynamic characteristics in pitch of several ring-wing-body configurations at a mach number of 2.2. Odell Morris.

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Pressure measurements on two 60° swept delta wings with blunt leading edges and dihedral angles of 0° and 45° at a Mach number of 4.95. Calvin Stainback.

Stainback, P. Calvin.
United States. National Aeronautics and Space Administration.

January 1962

Cover title."April 1962."Aerodynamics, aircraft; Aerodynamics, missiles; Fluid mechanics; Stresses a...

Flight investigation of some effects of a vane-controlled gust-alleviation system on the wing and tail loads fo a transport airplane /

Schott, Russell L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; St...

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...

Experimental investigation of a hypersonic glider configuration at a mach number of 6 and at full-scale Reynolds numbers /

Seiff, Alvin.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Stabil...

Effects of leading-edge bluntness on flutter characteristics of some square-planform double-wedge airfoils at a Mach number of 15.4 /

Goetz, Robert C.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Stresses and loads.Includes bi...

Investigation of vortex movements about a wing in intermediate and high subsonic flow undergoing a large angle-of-attack change in a blast-induced gust /

McFarland, Donald R.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Fluid mechanics; Stability and control.Includes bib...

A wind-tunnel investigation at a Mach number of 2.01 of the sonic-boom characteristics of three wing-body combinations differing in wing longitudinal location /

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise.Includes bi...

Experimental investigation of the effect of aspect ratio and Mach number on the flutter of cantilever wings /

Widmayer, E.
Clevenston, S. A.
Lauten, W. T.
Langley Research Center.

January 1960

"NASA TN D-229.""Langley Research Center, Langley Field, Va.""April 1960."Cover title.Includes bibli...

Theoretical calculations of the pressures, forces and moments due to various larteral motions acting on tapered sweptback vertical tails with superesonic leading and trainling edges /

Margolis, Kenneth.
Elliott, Miriam H.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and load...

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...

Analytical and experimental investigation of flutter and divergence of speed-mounted cone configurations at supersonic speeds / y John L. Sewall, Robert W. Hess and Charles E. Watkins.

Sewall, John L.
Watkins, Charles E.
Hess, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Stresses and lo...

Velocity potential and forces on oscillating slender bodies of revolution in supersoni flow expanded to the fifth power of the frequency /

Lansing, Donald L.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

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...

An investigation of the influence of lift on sonic-boom intensity by means of wind-tunnel measurements of the pressure fields of several wing-body combinations at a mach number of 2.01 /

Carlson, Harry W.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircraft ...

Aerodynamic characteristics in pitch of several ring-wing-body configurations at a mach number of 2.2. Odell Morris.

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Pressure measurements on two 60° swept delta wings with blunt leading edges and dihedral angles of 0° and 45° at a Mach number of 4.95. Calvin Stainback.

Stainback, P. Calvin.
United States. National Aeronautics and Space Administration.

January 1962

Cover title."April 1962."Aerodynamics, aircraft; Aerodynamics, missiles; Fluid mechanics; Stresses a...

Flight investigation of some effects of a vane-controlled gust-alleviation system on the wing and tail loads fo a transport airplane /

Schott, Russell L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; St...

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...

Experimental investigation of a hypersonic glider configuration at a mach number of 6 and at full-scale Reynolds numbers /

Seiff, Alvin.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Stabil...

Effects of leading-edge bluntness on flutter characteristics of some square-planform double-wedge airfoils at a Mach number of 15.4 /

Goetz, Robert C.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aerodynamics, missiles and space vehicles; Stresses and loads.Includes bi...

Investigation of vortex movements about a wing in intermediate and high subsonic flow undergoing a large angle-of-attack change in a blast-induced gust /

McFarland, Donald R.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Fluid mechanics; Stability and control.Includes bib...

A wind-tunnel investigation at a Mach number of 2.01 of the sonic-boom characteristics of three wing-body combinations differing in wing longitudinal location /

Morris, Odell A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise.Includes bi...

Experimental investigation of the effect of aspect ratio and Mach number on the flutter of cantilever wings /

Widmayer, E.
Clevenston, S. A.
Lauten, W. T.
Langley Research Center.

January 1960

"NASA TN D-229.""Langley Research Center, Langley Field, Va.""April 1960."Cover title.Includes bibli...

Theoretical calculations of the pressures, forces and moments due to various larteral motions acting on tapered sweptback vertical tails with superesonic leading and trainling edges /

Margolis, Kenneth.
Elliott, Miriam H.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and load...

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...

Analytical and experimental investigation of flutter and divergence of speed-mounted cone configurations at supersonic speeds / y John L. Sewall, Robert W. Hess and Charles E. Watkins.

Sewall, John L.
Watkins, Charles E.
Hess, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, missiles and space vehicles; Fluid mechanics; Stresses and lo...

Velocity potential and forces on oscillating slender bodies of revolution in supersoni flow expanded to the fifth power of the frequency /

Lansing, Donald L.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid me...

Experimental investigation of oscillatory aerodynamic forces, moments and pressures acting on a tapered wing oscillating in pitch at mach numbers from 0.40 to 1.07 /

Abstract

Extracted data

Experimental investigation of oscillatory aerodynamic forces, moments and pressures acting on a tapered wing oscillating in pitch at mach numbers from 0.40 to 1.07 /

Abstract

Extracted data

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