Investigation of a high-speed hydrofoil with parabolic thickness distribution /

Investigation of the rolling stability derivatives of two hypersonic gliders of parabolic plan form at high subsonic speeds /

Arabian, Donald D.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

The blunt plate in hypersonic flow /

Baradell, Donald L. (Donald Louis), 1933-
Bertram, Mitchel H.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid ...

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...

Experimental investigation of a high-speed hydrofoil with parabolic thickness distribution and an aspect ration of 3 /

Christopher, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Fluid mechanics;Includes bibliographical references.Mode of access: Interne...

Experimental investigation of aspect ratio 1 supercavitating hydrofoils at speeds up to 185 feet per second /

Christopher, Kenneth W.
Johnson, Virgil E.
United States. National Aeronautics and Space Administration.

Cover title."January 1960."Wing-section theory; Wing sections, camber; Hydrodynamic theory; Hydrofoi...

A hydrodynamic investigation of the effect of adding upper-surface camber to a submerged flat plate /

Vaughan, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."November 1959."Wing sections, camber; Wing sections, thickness; Hydrodynamic configurat...

Hydrodynamic and aerodynamic characteristics of a model of a supersonic multijet water-based aircraft equipped with supercavitating hydrofoils /

McKann, Robert E.
Pearson, Albin O.
Blanchard, Ulysse J.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Low-speed investigation of a full-span internal-flow jet-augmented flap on a high-wing model with a 35 degree swept wing of aspect ratio 7.0 /

Turner, Thomas R.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft, Aircraft; Stability and control.Includes bibliogra...

Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bibl...

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 exploratory study of a parawing as a high-lift device for aircraft /

Naeseth, Rodger L.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

High-subsonic-speed investigation of the static longitudinal aerodynamic characteristics of several delta-wing configurations for angles of attack from 0° to 90° /

Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"December 1959."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds /

Savin, Raymond C.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "September 15, 1958."Includes bibliographical references: p. 35-36.Mode of access: I...

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...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

January 1959

Cover title."October 1959."Includes bibliographical references.Mode of access: Internet

Investigation of the rolling stability derivatives of two hypersonic gliders of parabolic plan form at high subsonic speeds /

Arabian, Donald D.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

The blunt plate in hypersonic flow /

Baradell, Donald L. (Donald Louis), 1933-
Bertram, Mitchel H.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid ...

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...

Experimental investigation of a high-speed hydrofoil with parabolic thickness distribution and an aspect ration of 3 /

Christopher, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Fluid mechanics;Includes bibliographical references.Mode of access: Interne...

Experimental investigation of aspect ratio 1 supercavitating hydrofoils at speeds up to 185 feet per second /

Christopher, Kenneth W.
Johnson, Virgil E.
United States. National Aeronautics and Space Administration.

Cover title."January 1960."Wing-section theory; Wing sections, camber; Hydrodynamic theory; Hydrofoi...

A hydrodynamic investigation of the effect of adding upper-surface camber to a submerged flat plate /

Vaughan, Victor L.
United States. National Aeronautics and Space Administration.

Cover title."November 1959."Wing sections, camber; Wing sections, thickness; Hydrodynamic configurat...

Hydrodynamic and aerodynamic characteristics of a model of a supersonic multijet water-based aircraft equipped with supercavitating hydrofoils /

McKann, Robert E.
Pearson, Albin O.
Blanchard, Ulysse J.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Low-speed investigation of a full-span internal-flow jet-augmented flap on a high-wing model with a 35 degree swept wing of aspect ratio 7.0 /

Turner, Thomas R.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft, Aircraft; Stability and control.Includes bibliogra...

Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bibl...

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 exploratory study of a parawing as a high-lift device for aircraft /

Naeseth, Rodger L.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

High-subsonic-speed investigation of the static longitudinal aerodynamic characteristics of several delta-wing configurations for angles of attack from 0° to 90° /

Spencer, Bernard, 1932-
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"December 1959."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds /

Savin, Raymond C.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "September 15, 1958."Includes bibliographical references: p. 35-36.Mode of access: I...

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...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

January 1959

Cover title."October 1959."Includes bibliographical references.Mode of access: Internet

Investigation of the rolling stability derivatives of two hypersonic gliders of parabolic plan form at high subsonic speeds /

Arabian, Donald D.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

The blunt plate in hypersonic flow /

Baradell, Donald L. (Donald Louis), 1933-
Bertram, Mitchel H.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid ...

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...

Investigation of a high-speed hydrofoil with parabolic thickness distribution /

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Investigation of a high-speed hydrofoil with parabolic thickness distribution /

Abstract

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