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

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

Margason, Richard J. (Richard John), 1936-
Gentry, Garl L., Jr.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Research prepared at Langley Research Center.N68-36081.Cover title.Includes bibliographical referenc...

Simulator evaluation of the low-speed flying qualities of an experimental STOL configuration with an externally blown flap wing or an augmentor wing /

Powers, Bruce G.
Kier, David A.
Flight Research Center (U.S.)

January 1973

Prepared at the NASA Flight Research Center.Cover title.Includes bibliographical references (p. 17-1...

A brief study of the effects of turbofan-engine bypass ratio on short- and long-haul cruise aircraft /

Keith, Arvid L.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ...

The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model /

Heyson, Harry H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 66-69).Mode ...

Aerodynamic effects of five lift-fan pod arrangements on an unpowered V/STOL transport model /

Thomas, James L. (James Lee), 1952-
Croom, Delwin R.
Hoad, Danny R.
Langley Research Center.

January 1973

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

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 ...

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 ...

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

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Investigation of the static lift capability of a low-aspect-ratio wing operating in a powered ground-effect mode /

Huffman, Jarrett K.
Jackson, Charlie M.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 3).Mode of a...

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 ...

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

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

Calculation of the twist distribution of wings designed for cruise at transonic speeds /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

A Study of the effect of flight density and background noise on V/STOL acceptability /

Sternfeld, Harry.
Langley Research Center.
Boeing Vertol Company.

January 1974

"Prepared by Boeing Vertol Company ... for Langley Research Center."Cover title.Bibliography: p. 55....

Transonic flutter study of a 50.5 ̊cropped-delta wing with two rearward-mounted nacelles /

Sandford, M. C. (Maynard C.)
Abel, Irving.
Ruhlin, Charles L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

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

Margason, Richard J. (Richard John), 1936-
Gentry, Garl L., Jr.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Research prepared at Langley Research Center.N68-36081.Cover title.Includes bibliographical referenc...

Simulator evaluation of the low-speed flying qualities of an experimental STOL configuration with an externally blown flap wing or an augmentor wing /

Powers, Bruce G.
Kier, David A.
Flight Research Center (U.S.)

January 1973

Prepared at the NASA Flight Research Center.Cover title.Includes bibliographical references (p. 17-1...

A brief study of the effects of turbofan-engine bypass ratio on short- and long-haul cruise aircraft /

Keith, Arvid L.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ...

The effect of wind-tunnel wall interference on the performance of a fan-in-wing VTOL model /

Heyson, Harry H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 66-69).Mode ...

Aerodynamic effects of five lift-fan pod arrangements on an unpowered V/STOL transport model /

Thomas, James L. (James Lee), 1952-
Croom, Delwin R.
Hoad, Danny R.
Langley Research Center.

January 1973

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

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 ...

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 ...

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

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Investigation of the static lift capability of a low-aspect-ratio wing operating in a powered ground-effect mode /

Huffman, Jarrett K.
Jackson, Charlie M.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 3).Mode of a...

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 ...

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

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

Calculation of the twist distribution of wings designed for cruise at transonic speeds /

Mann, Michael J.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode ...

A Study of the effect of flight density and background noise on V/STOL acceptability /

Sternfeld, Harry.
Langley Research Center.
Boeing Vertol Company.

January 1974

"Prepared by Boeing Vertol Company ... for Langley Research Center."Cover title.Bibliography: p. 55....

Transonic flutter study of a 50.5 ̊cropped-delta wing with two rearward-mounted nacelles /

Sandford, M. C. (Maynard C.)
Abel, Irving.
Ruhlin, Charles L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

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

Margason, Richard J. (Richard John), 1936-
Gentry, Garl L., Jr.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Research prepared at Langley Research Center.N68-36081.Cover title.Includes bibliographical referenc...

Simulator evaluation of the low-speed flying qualities of an experimental STOL configuration with an externally blown flap wing or an augmentor wing /

Powers, Bruce G.
Kier, David A.
Flight Research Center (U.S.)

January 1973

Prepared at the NASA Flight Research Center.Cover title.Includes bibliographical references (p. 17-1...

A brief study of the effects of turbofan-engine bypass ratio on short- and long-haul cruise aircraft /

Keith, Arvid L.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ...

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

Abstract

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

Abstract

Extracted data

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