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

Hypersonic aerodynamic characteristics of minimum-wave-drag bodies having variations in cross-sectional shape /

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

January 1967

Cover title."September 1967."Includes bibliographical references (p. 10).Mode of access: Internet

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 a high-speed hydrofoil with parabolic thickness distribution /

Johnson, Virgil E.
Rasnick, Thomas A.
United States. National Aeronautics and Space Administration.

Cover title."November 1959."Wing-section theory; Wing sections, camber; Wings, complete, aspect rati...

Aerodynamic and hydrodynamic characteristics of a proposed supersonic multijet water-based hull-type airplane with a variable-incidence wing /

Petynia, William W.
Fournier, Roger H.
Pearson, Albin O.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Transonic aerodynamic characteristics of a model of a proposed six-engine hull-type seaplane designed for supersonic flight /

Wornom, Dewey E.
United States. National Aeronautics and Space Administration.

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

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack /

Bielat, Ralph P.
Alford, William J.
Robins, A. Warner.
Langley Research Center.

January 1960

"August 1960."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Aerodynamic characteristics of a large-scale model with a high disk-loading lifting fan mounted in the fuselage /

Aoyagi, Kiyoshi.
deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode...

Water-landing characteristics of a 1/10-scale model of a winged missile /

Fisher, Lloyd J.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Aerodynamic characteristics of a three-engine supersonic transport model having a low-aspect-ratio variable-sweep warped wing /

Morris, Odell A.
Fuller, Dennis E.
Langley Research Center.

January 1964

"September 1964."Includes bibliographical references (p. 9).Mode of access: Internet

Low-speed aerodynamic characteristics of a model of a hypersonic research airplane at angles of attack up to 90 degrees for a range of Reynolds numbers /

Bowman, James S.
Grantham, William D.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft;Aircraft; Stability and control;Includes biblio...

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...

Experimental and calculated flow fields produced by airplanes flying at supersonic speeds /

Smith, Harriet J.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics aircraft; Aircraft safety and noise.Includes bibliographica...

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...

Hypersonic aerodynamic characteristics of minimum-wave-drag bodies having variations in cross-sectional shape /

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

January 1967

Cover title."September 1967."Includes bibliographical references (p. 10).Mode of access: Internet

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 a high-speed hydrofoil with parabolic thickness distribution /

Johnson, Virgil E.
Rasnick, Thomas A.
United States. National Aeronautics and Space Administration.

Cover title."November 1959."Wing-section theory; Wing sections, camber; Wings, complete, aspect rati...

Aerodynamic and hydrodynamic characteristics of a proposed supersonic multijet water-based hull-type airplane with a variable-incidence wing /

Petynia, William W.
Fournier, Roger H.
Pearson, Albin O.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

Transonic aerodynamic characteristics of a model of a proposed six-engine hull-type seaplane designed for supersonic flight /

Wornom, Dewey E.
United States. National Aeronautics and Space Administration.

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

Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds /

Fournier, Paul G.
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliog...

Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable-sweep wing having a free-floating apex /

Polhamus, Edward C., 1948-
Hammond, Alexander D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1965

"July 1965"--Cover.Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack /

Bielat, Ralph P.
Alford, William J.
Robins, A. Warner.
Langley Research Center.

January 1960

"August 1960."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Aerodynamic characteristics of a large-scale model with a high disk-loading lifting fan mounted in the fuselage /

Aoyagi, Kiyoshi.
deSavigny, Richard A.
Hickey, David H.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode...

Water-landing characteristics of a 1/10-scale model of a winged missile /

Fisher, Lloyd J.
United States. National Aeronautics and Space Administration.

Cover title."April 1967."Includes bibliographical references.Mode of access: Internet

Aerodynamic characteristics of a three-engine supersonic transport model having a low-aspect-ratio variable-sweep warped wing /

Morris, Odell A.
Fuller, Dennis E.
Langley Research Center.

January 1964

"September 1964."Includes bibliographical references (p. 9).Mode of access: Internet

Low-speed aerodynamic characteristics of a model of a hypersonic research airplane at angles of attack up to 90 degrees for a range of Reynolds numbers /

Bowman, James S.
Grantham, William D.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft;Aircraft; Stability and control;Includes biblio...

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...

Experimental and calculated flow fields produced by airplanes flying at supersonic speeds /

Smith, Harriet J.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics aircraft; Aircraft safety and noise.Includes bibliographica...

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...

Hypersonic aerodynamic characteristics of minimum-wave-drag bodies having variations in cross-sectional shape /

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

January 1967

Cover title."September 1967."Includes bibliographical references (p. 10).Mode of access: Internet

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 a high-speed hydrofoil with parabolic thickness distribution /

Johnson, Virgil E.
Rasnick, Thomas A.
United States. National Aeronautics and Space Administration.

Cover title."November 1959."Wing-section theory; Wing sections, camber; Wings, complete, aspect rati...

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

Abstract

Extracted data

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

Abstract

Extracted data

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