Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Aerodynamic characteristics of a large aircraft to transport space shuttle orbiter or other external payloads /

Paulson, John W.
Langley Research Center.

January 1975

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

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

Dynamics and identification on flexible aircraft /

Wells, William R.
United States. National Aeronautics and Space Administration.
University of Cincinnati. Dept. of Aerospace Engineering.

January 1976

Cover title.Includes bibliographical references (p. 52).Mode of access: Internet

Effect of rotor wake on aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft /

Mineck, Raymond E.
United States. National Aeronautics and Space Administration.

January 1977

Issued Sept. 1977.Includes bibliographical references (p. 14).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...

On the formulation of the aerodynamic characteristics in aircraft dynamics /

Tobak, Murray.
Schiff, Lewis B.
Ames Research Center.

January 1976

Prepared at Ames Research Center."Corrected copy."Cover title.Includes bibliographical references (p...

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...

Effect of advanced rotorcraft airfoil sections on the hover performance of a small-scale rotor model /

Althoff, Susan L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"September 1988"--Cover.Includes bibliographical references (p. 7-8).Mode of access: Internet

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

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

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...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Some recent studies in structural dynamics of rotor aircraft /

Brooks, George W.
Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Investigation of the aerodynamic characteristics of a 0.067-scale model of the x-15 airplane (configuration 3) at mach numbers of 2.29, 2.98, and 4.65 /

Franklin, Arthur E.
Lust, Robert M.
Langley Research Center.

January 1959

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

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

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

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

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...

Aerodynamic characteristics of a large aircraft to transport space shuttle orbiter or other external payloads /

Paulson, John W.
Langley Research Center.

January 1975

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

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

Dynamics and identification on flexible aircraft /

Wells, William R.
United States. National Aeronautics and Space Administration.
University of Cincinnati. Dept. of Aerospace Engineering.

January 1976

Cover title.Includes bibliographical references (p. 52).Mode of access: Internet

Effect of rotor wake on aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft /

Mineck, Raymond E.
United States. National Aeronautics and Space Administration.

January 1977

Issued Sept. 1977.Includes bibliographical references (p. 14).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...

On the formulation of the aerodynamic characteristics in aircraft dynamics /

Tobak, Murray.
Schiff, Lewis B.
Ames Research Center.

January 1976

Prepared at Ames Research Center."Corrected copy."Cover title.Includes bibliographical references (p...

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...

Effect of advanced rotorcraft airfoil sections on the hover performance of a small-scale rotor model /

Althoff, Susan L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"September 1988"--Cover.Includes bibliographical references (p. 7-8).Mode of access: Internet

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

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

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...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Some recent studies in structural dynamics of rotor aircraft /

Brooks, George W.
Silveira, Milton A.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stresses and loads.Includes bibliogr...

Investigation of the aerodynamic characteristics of a 0.067-scale model of the x-15 airplane (configuration 3) at mach numbers of 2.29, 2.98, and 4.65 /

Franklin, Arthur E.
Lust, Robert M.
Langley Research Center.

January 1959

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

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

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

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

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...

Aerodynamic characteristics of a large aircraft to transport space shuttle orbiter or other external payloads /

Paulson, John W.
Langley Research Center.

January 1975

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

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

Dynamics and identification on flexible aircraft /

Wells, William R.
United States. National Aeronautics and Space Administration.
University of Cincinnati. Dept. of Aerospace Engineering.

January 1976

Cover title.Includes bibliographical references (p. 52).Mode of access: Internet

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Abstract

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Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Abstract

Extracted data

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