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

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...

Some effects of tip fins of wing flutter characteristics /

Goetz, Robert C. (Robert Charles), 1937-
Doggett, Robert V.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode ...

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 ...

Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 /

Rumsey, Charles B. (Charles Bertrand)
Hopko, Russell N.
Piland, Robert Owens.
Langley Research Center.

Prepared at Langley Research Center."January 1960."Cover title.Includes bibliographical references (...

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...

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...

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 ...

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...

Investigation of effects of roughness, surface cooling, and shock impingement on boundary-layer transition on a two-dimensional wing /

Czarnecki, K. R.
Sevier, John R.
United States. National Aeronautics and Space Administration.

Cover title."June 1960."Flow, laminar; Flow, turbulent; Aerodynamics with heat; Surface conditions,...

A method for calculating aerodynamic loadings on thin wings at a Mach number of 1 /

Crigler, John L.
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

Supersonic flutter of panels loaded with inplane shear /

Sawyer, James Wayne, 1941-
Langely Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ...

Flutter of aerodynamically heated aluminum-alloy and stainless-steel panels with length-width ratio of 10 at mach number of 3.0 / Lawrence D. Guy and Herman L. Bohon.

Guy, Lawrence D. (Lawrence Duncan), 1921-
Bohon, Herman L.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Stresses and loads.Includes bibliographical references.Mode of access: Inter...

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...

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

The aerodynamic characteristics of a body in the flow field near the tip of a circular-arc wing of rectangular plan form at a mach number of 2.01 /

Gapcynski, John P.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

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...

Some effects of tip fins of wing flutter characteristics /

Goetz, Robert C. (Robert Charles), 1937-
Doggett, Robert V.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode ...

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 ...

Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 /

Rumsey, Charles B. (Charles Bertrand)
Hopko, Russell N.
Piland, Robert Owens.
Langley Research Center.

Prepared at Langley Research Center."January 1960."Cover title.Includes bibliographical references (...

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...

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...

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 ...

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...

Investigation of effects of roughness, surface cooling, and shock impingement on boundary-layer transition on a two-dimensional wing /

Czarnecki, K. R.
Sevier, John R.
United States. National Aeronautics and Space Administration.

Cover title."June 1960."Flow, laminar; Flow, turbulent; Aerodynamics with heat; Surface conditions,...

A method for calculating aerodynamic loadings on thin wings at a Mach number of 1 /

Crigler, John L.
Langley Research Center.

Prepared at Langley Research Center."November 1959."Cover title.Includes bibliographical references ...

Supersonic flutter of panels loaded with inplane shear /

Sawyer, James Wayne, 1941-
Langely Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16).Mode of ...

Flutter of aerodynamically heated aluminum-alloy and stainless-steel panels with length-width ratio of 10 at mach number of 3.0 / Lawrence D. Guy and Herman L. Bohon.

Guy, Lawrence D. (Lawrence Duncan), 1921-
Bohon, Herman L.
United States. National Aeronautics and Space Administration.

Cover title."July 1962."Stresses and loads.Includes bibliographical references.Mode of access: Inter...

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...

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

The aerodynamic characteristics of a body in the flow field near the tip of a circular-arc wing of rectangular plan form at a mach number of 2.01 /

Gapcynski, John P.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 7).Mode of access: Internet

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...

Some effects of tip fins of wing flutter characteristics /

Goetz, Robert C. (Robert Charles), 1937-
Doggett, Robert V.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode ...

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 ...

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

Abstract

Extracted data

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

Abstract

Extracted data

Related items

Related items