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

Experimental investigation of the pressure fluctuations on a flat plate and a cylinder in the slipstream of a hovering rotor /

McKee, John W.
Langley Research Center.

January 1959

"NASA TN D-112.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Inclu...

The effects of winglets on low aspect ratio wings at supersonic Mach numbers /

Keenan, James A. (James Anthony), 1966-
Kuhlman, John, 1948-
Langley Research Center.
West Virginia University. Dept. of Mechanical and Aerospace Engineering.

January 1991

Prepared at the Dept. of Mechanical and Aerospace Engineering, West Virginia University, for Langley...

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...

An experimental study of the flutter of sails having a delta planform tested from a Mach number of 0.1 to a Mach number of 1.9 /

Hess, R. W. (Robert W.)
Langley Research Center.
United States. National Aeronautics and Space Administration.

"Langley Research Center, Langely Field, Va.""March 1961."Cover title.Includes bibliographical refer...

Effect of aerodynamic heating on the flutter of a rectangular wing at a mach number of 2 /

Runyan, Harry L.
Jones, Nan H.
Langley Research Center.

Prepared at the Langley Research Center, Langley Research Center.Cover title."June 1960."--Cover.Inc...

Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model /

Ruhlin, Charles L.
Nagaraja, K. S.
Bhatia, Kumar G. (Kumar Gobindram), 1941-
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 2...

An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics /

Doggett, Robert V.
Morgan, Homer G.
Rainey, A. Gerald.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

An examination of methods of buffeting analysis based on experiments with wings of varying stiffness /

Rainey, A. Gerald.
Byrdsong, Thomas A.
Langley Research Center.

January 1959

"NASA TN D-3.""Langley Research Center, Langley Field, Va.""August 1959."Cover title.Includes biblio...

Use of experimental steady-flow aerodynamic parameters in the calculation of flutter characteristics for finite-span swept or unswept wings at subsonic, transonic, and supersonic speed /

Yates, E. Carson (Edward Carson), 1926-
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 19-20).Mode of access: Internet

Effects of a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 /

Landrum, Emma Jean.
Langley Research Center.

January 1960

"NASA TN D-183.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes ...

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 /

Leadbetter, Sumner A.
Igoe, William B.
Clevenson, Sherman A.
United States. National Aeronautics and Space Administration.

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

Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by the free-oscillation method /

Tuovila, W. J. (Weimer J.)
Hess, R. W. (Robert W.)
Langley Research Center.

January 1960

"NASA TN D-116.""Langley Research Center, Langley Field, Va.""February 1960."Title from cover.Includ...

Investigation at transonic speeds to determine lateral control effectiveness of blowing laterally over surfaces of 30° and 45° swept wings /

Hammond, Alexander D.
McKinney, Linwood W.
Langley Research Center.

January 1959

"NASA TN D-42.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Includes...

Experimental and analytical investigation of flutter of a nonuniform sweptback cantilever wing with two concentrated weights /

Sewall, John L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"December 4, 1951."Includes bibliographical references (p. 17).Mode of access: Internet

Aerodynamic and flow-visualization studies of variations in the geometry of irregular planform wings at a Mach number of 20.3 /

Stone, David R. (David Ray)
Spencer, Bernard, 1932-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Experimental investigation of the pressure fluctuations on a flat plate and a cylinder in the slipstream of a hovering rotor /

McKee, John W.
Langley Research Center.

January 1959

"NASA TN D-112.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Inclu...

The effects of winglets on low aspect ratio wings at supersonic Mach numbers /

Keenan, James A. (James Anthony), 1966-
Kuhlman, John, 1948-
Langley Research Center.
West Virginia University. Dept. of Mechanical and Aerospace Engineering.

January 1991

Prepared at the Dept. of Mechanical and Aerospace Engineering, West Virginia University, for Langley...

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...

An experimental study of the flutter of sails having a delta planform tested from a Mach number of 0.1 to a Mach number of 1.9 /

Hess, R. W. (Robert W.)
Langley Research Center.
United States. National Aeronautics and Space Administration.

"Langley Research Center, Langely Field, Va.""March 1961."Cover title.Includes bibliographical refer...

Effect of aerodynamic heating on the flutter of a rectangular wing at a mach number of 2 /

Runyan, Harry L.
Jones, Nan H.
Langley Research Center.

Prepared at the Langley Research Center, Langley Research Center.Cover title."June 1960."--Cover.Inc...

Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model /

Ruhlin, Charles L.
Nagaraja, K. S.
Bhatia, Kumar G. (Kumar Gobindram), 1941-
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 2...

An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics /

Doggett, Robert V.
Morgan, Homer G.
Rainey, A. Gerald.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

An examination of methods of buffeting analysis based on experiments with wings of varying stiffness /

Rainey, A. Gerald.
Byrdsong, Thomas A.
Langley Research Center.

January 1959

"NASA TN D-3.""Langley Research Center, Langley Field, Va.""August 1959."Cover title.Includes biblio...

Use of experimental steady-flow aerodynamic parameters in the calculation of flutter characteristics for finite-span swept or unswept wings at subsonic, transonic, and supersonic speed /

Yates, E. Carson (Edward Carson), 1926-
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 19-20).Mode of access: Internet

Effects of a lower surface jet on the lift-drag ratio of a 45° sweptback wing at a Mach number of 2.01 /

Landrum, Emma Jean.
Langley Research Center.

January 1960

"NASA TN D-183.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes ...

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 /

Leadbetter, Sumner A.
Igoe, William B.
Clevenson, Sherman A.
United States. National Aeronautics and Space Administration.

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

Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by the free-oscillation method /

Tuovila, W. J. (Weimer J.)
Hess, R. W. (Robert W.)
Langley Research Center.

January 1960

"NASA TN D-116.""Langley Research Center, Langley Field, Va.""February 1960."Title from cover.Includ...

Investigation at transonic speeds to determine lateral control effectiveness of blowing laterally over surfaces of 30° and 45° swept wings /

Hammond, Alexander D.
McKinney, Linwood W.
Langley Research Center.

January 1959

"NASA TN D-42.""Langley Research Center, Langley Field, Va.""October 1959."Title from cover.Includes...

Experimental and analytical investigation of flutter of a nonuniform sweptback cantilever wing with two concentrated weights /

Sewall, John L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"December 4, 1951."Includes bibliographical references (p. 17).Mode of access: Internet

Aerodynamic and flow-visualization studies of variations in the geometry of irregular planform wings at a Mach number of 20.3 /

Stone, David R. (David Ray)
Spencer, Bernard, 1932-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Experimental investigation of the pressure fluctuations on a flat plate and a cylinder in the slipstream of a hovering rotor /

McKee, John W.
Langley Research Center.

January 1959

"NASA TN D-112.""Langley Research Center, Langley Field, Va.""September 1959."Title from cover.Inclu...

The effects of winglets on low aspect ratio wings at supersonic Mach numbers /

Keenan, James A. (James Anthony), 1966-
Kuhlman, John, 1948-
Langley Research Center.
West Virginia University. Dept. of Mechanical and Aerospace Engineering.

January 1991

Prepared at the Dept. of Mechanical and Aerospace Engineering, West Virginia University, for Langley...

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...

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

Abstract

Extracted data

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

Abstract

Extracted data

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