Unsteady aerodynamics for advanced configurations.

Flutter analysis and testing of pairs of aerodynamically interfering delta wings /

Chipman, Richard R.
Rauch, Frank J.
Langley Research Center.
Grumman Aerospace Corporation.

January 1973

"Prepared by Grumann Aerospace Corporation ... for Langley Research Center."Cover title.Bibliography...

Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Ashby, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

Design trends for Army/Air Force airplanes in the United States /

Spearman, M. Leroy.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Includes bibliographical references (p. 18-19).Mode of access: I...

Unsteady aerodynamics for advanced configurations.

Moore, M. T., author.
Andrew, L. V., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
North American Aviation. Space and Information Systems Division. sponsor.

"May 1965."Includes bibliograpical references (pages 61-62).Air Force Contract No.Mode of access: In...

Simple aerodynamics and the airplane,

Monteith, Charles Norton, 1893-1940.
Carter, Clifton Carroll, 1876-1950.
Aldrin, Edwin Eugene, 1896-

Earlier editions, published officially, are entered under the heading U. S. Office of chief of Air ...

An analytical technique for approximating unsteady aerodynamics in the time domain / H.J. Dunn.

Dunn, H. J., 1947-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Includes bibliographical references.Nov. 1980."Langley Research Center."Mode of access: Internet

Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls.

Kaufman, Louis G., II., author.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
Wright-Patterson Air Force Base. Flight Dynamics Laboratory. Research and Technology Division. issuing body.
Grumman Aircraft Engineering Corporation. sponsor.

Includes bibliograpical references (page 4).Air Force Contract No.Mode of access: Internet

In-flight investigation of the effects of higher-order control system dynamics on longitudinal handling qualities /

Di Franco, Dante A., author.
Cornell Aeronautical Laboratory. sponsor.
Air Force Flight Dynamics Laboratory (U.S.). issuing body.
Air Force Wright Aeronautical Laboratories. sponsor.

Includes bibliographicsl references (page 178).Print reproduction.Air Force Contract No.Mode of acce...

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

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 ...

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

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...

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

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

An analytical study and wind-tunnel tests of an aeromechanical gust-alleviation system for a light airplane /

Stewart, Eric C.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 44).Mode of ...

Flutter analysis and testing of pairs of aerodynamically interfering delta wings /

Chipman, Richard R.
Rauch, Frank J.
Langley Research Center.
Grumman Aerospace Corporation.

January 1973

"Prepared by Grumann Aerospace Corporation ... for Langley Research Center."Cover title.Bibliography...

Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Ashby, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

Design trends for Army/Air Force airplanes in the United States /

Spearman, M. Leroy.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Includes bibliographical references (p. 18-19).Mode of access: I...

Unsteady aerodynamics for advanced configurations.

Moore, M. T., author.
Andrew, L. V., author.
United States. Air Force. Systems Command. issuing body.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
North American Aviation. Space and Information Systems Division. sponsor.

"May 1965."Includes bibliograpical references (pages 61-62).Air Force Contract No.Mode of access: In...

Simple aerodynamics and the airplane,

Monteith, Charles Norton, 1893-1940.
Carter, Clifton Carroll, 1876-1950.
Aldrin, Edwin Eugene, 1896-

Earlier editions, published officially, are entered under the heading U. S. Office of chief of Air ...

An analytical technique for approximating unsteady aerodynamics in the time domain / H.J. Dunn.

Dunn, H. J., 1947-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Includes bibliographical references.Nov. 1980."Langley Research Center."Mode of access: Internet

Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls.

Kaufman, Louis G., II., author.
Air Force Flight Dynamics Laboratory (U.S.). sponsor.
Wright-Patterson Air Force Base. Flight Dynamics Laboratory. Research and Technology Division. issuing body.
Grumman Aircraft Engineering Corporation. sponsor.

Includes bibliograpical references (page 4).Air Force Contract No.Mode of access: Internet

In-flight investigation of the effects of higher-order control system dynamics on longitudinal handling qualities /

Di Franco, Dante A., author.
Cornell Aeronautical Laboratory. sponsor.
Air Force Flight Dynamics Laboratory (U.S.). issuing body.
Air Force Wright Aeronautical Laboratories. sponsor.

Includes bibliographicsl references (page 178).Print reproduction.Air Force Contract No.Mode of acce...

Analysis of transonic flow about lifting wing-body configurations /

Barnwell, Richard W.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 69-71).Mode ...

Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient /

Bingham, Gene J.
Chen, Allen Wen-shin, 1945-
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 13.Mode of access: Internet

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 ...

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

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...

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

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

An analytical study and wind-tunnel tests of an aeromechanical gust-alleviation system for a light airplane /

Stewart, Eric C.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 44).Mode of ...

Flutter analysis and testing of pairs of aerodynamically interfering delta wings /

Chipman, Richard R.
Rauch, Frank J.
Langley Research Center.
Grumman Aerospace Corporation.

January 1973

"Prepared by Grumann Aerospace Corporation ... for Langley Research Center."Cover title.Bibliography...

Aerodynamic testing technique for twin-fuselage models at hypersonic speeds /

Ashby, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 6).Mode of a...

Design trends for Army/Air Force airplanes in the United States /

Spearman, M. Leroy.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Includes bibliographical references (p. 18-19).Mode of access: I...

Unsteady aerodynamics for advanced configurations.

Abstract

Extracted data

Unsteady aerodynamics for advanced configurations.

Abstract

Extracted data

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