Aerodynamic characteristics of a five-jet VTOL configuration in the transition speed range /

wind-tunnel investigation of longitudinal aerodynamic characteristics of three propeller-driven VTOL configurations in the transition speed range, including effects of ground proximity /

Kuhn, Richard E.
Hayes, William C.
United States. National Aeronautics and Space Administration.

Cover title."February 1960."Flaps, trailing-edge, complete wings; Slipstream, propellers; Tail-wing-...

Longitudinal aerodynamic characteristics of a generic fighter model with a wing designed for sustained transonic maneuver conditions /

Ferris, James C.
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986."Includes bibliographical references (p. 39).Mode...

Low-speed wind-tunnel investigation of flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration /

Coe, Paul L.
Owens, D. B. (Donald Bruce), 1922-
Turner, Steven G. (Steven George)
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Longitudinal and lateral stability characteristics of two four-jet vtol models in the transition speed range /

Vogler, Raymond D.
Kuhn, Richard E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"May 1965."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Theoretical and experimental investigation of the performance of a fan-in-wing VTOL configuration /

Heyson, Harry H.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 32-34).Mode ...

Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 ̊swept delta wing /

Penland, Jim A.
Howard, Floyd G.
Creel, Theodore R.
Langley Research Center.

January 1974

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...

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

Aerodynamic characteristics of a five jet VTOL configuration in the transition speed range

Gentry, G. L., Jr.
Margason, R. J.

October 1968

Wind tunnel tests of a VTOL jet fighter to determine aerodynamic characteristics including stabilit

Pressure distribution on a vectored-thrust V/STOL fighter in the transition-speed range /

Mineck, Raymond E.
Margason, Richard J. (Richard John), 1936-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 11.Mode of access: Internet

Wind-tunnel investigation of steady-state aerodynamics of a composite-lift VTOL aircraft model /

Winston, Matthew M.
Huston, Robert J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Prepared at Langley Research Center.N69-28097.Cover title.Includes bibliographical references (p. 9)...

Aerodynamic characteristics of four-duct tandem VTOL-aircraft configurations /

Newsom, William A.
United States. National Aeronautics and Space Administration.

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

Hypersonic aerodynamic characteristics of a family of power-law, wing-body configuratioons /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 33-34).Mode ...

Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings /

Kelly, James R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 22.Mode of access: Internet

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /

Mack, Robert J.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 10-1...

wind-tunnel investigation of longitudinal aerodynamic characteristics of three propeller-driven VTOL configurations in the transition speed range, including effects of ground proximity /

Kuhn, Richard E.
Hayes, William C.
United States. National Aeronautics and Space Administration.

Cover title."February 1960."Flaps, trailing-edge, complete wings; Slipstream, propellers; Tail-wing-...

Longitudinal aerodynamic characteristics of a generic fighter model with a wing designed for sustained transonic maneuver conditions /

Ferris, James C.
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986."Includes bibliographical references (p. 39).Mode...

Low-speed wind-tunnel investigation of flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration /

Coe, Paul L.
Owens, D. B. (Donald Bruce), 1922-
Turner, Steven G. (Steven George)
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Longitudinal and lateral stability characteristics of two four-jet vtol models in the transition speed range /

Vogler, Raymond D.
Kuhn, Richard E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"May 1965."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Theoretical and experimental investigation of the performance of a fan-in-wing VTOL configuration /

Heyson, Harry H.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 32-34).Mode ...

Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 ̊swept delta wing /

Penland, Jim A.
Howard, Floyd G.
Creel, Theodore R.
Langley Research Center.

January 1974

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...

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

Aerodynamic characteristics of a five jet VTOL configuration in the transition speed range

Gentry, G. L., Jr.
Margason, R. J.

October 1968

Wind tunnel tests of a VTOL jet fighter to determine aerodynamic characteristics including stabilit

Pressure distribution on a vectored-thrust V/STOL fighter in the transition-speed range /

Mineck, Raymond E.
Margason, Richard J. (Richard John), 1936-
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 11.Mode of access: Internet

Wind-tunnel investigation of steady-state aerodynamics of a composite-lift VTOL aircraft model /

Winston, Matthew M.
Huston, Robert J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Prepared at Langley Research Center.N69-28097.Cover title.Includes bibliographical references (p. 9)...

Aerodynamic characteristics of four-duct tandem VTOL-aircraft configurations /

Newsom, William A.
United States. National Aeronautics and Space Administration.

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

Hypersonic aerodynamic characteristics of a family of power-law, wing-body configuratioons /

Townsend, James C. (James Courtland), 1938-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 33-34).Mode ...

Flight investigation of manual and automatic VTOL decelerating instrument approaches and landings /

Kelly, James R.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Bibliography: p. 22.Mode of access: Internet

Aerodynamic characteristics of wings designed with a combined-theory method to cruise at a Mach number of 4.5 /

Mack, Robert J.
Langley Research Center.

January 1988

Prepared at Langley Research Center."April 1988"--Cover.Includes bibliographical references (p. 10-1...

wind-tunnel investigation of longitudinal aerodynamic characteristics of three propeller-driven VTOL configurations in the transition speed range, including effects of ground proximity /

Kuhn, Richard E.
Hayes, William C.
United States. National Aeronautics and Space Administration.

Cover title."February 1960."Flaps, trailing-edge, complete wings; Slipstream, propellers; Tail-wing-...

Longitudinal aerodynamic characteristics of a generic fighter model with a wing designed for sustained transonic maneuver conditions /

Ferris, James C.
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986."Includes bibliographical references (p. 39).Mode...

Low-speed wind-tunnel investigation of flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration /

Coe, Paul L.
Owens, D. B. (Donald Bruce), 1922-
Turner, Steven G. (Steven George)
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 12.Mode of access: Internet

Aerodynamic characteristics of a five-jet VTOL configuration in the transition speed range /

Abstract

Extracted data

Aerodynamic characteristics of a five-jet VTOL configuration in the transition speed range /

Abstract

Extracted data

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