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

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

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

An analytical study of the effects of jets located more than one jet diameter above a wing at subsonic speeds /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1974

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

Results of full-scale wind tunnel tests on the H.126 jet flap aircraft /

Aiken, Thomas N.
Cook, Anthony, M.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Bibliography: p. 4.Mode of access: Internet

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 ...

Lowspeed wind-tunnel investigation of a semispan STOL jet transport wing-body with an upper-surface blown jet flap /

Phelps, Arthur R.
Henderson, Robert L.
Letko, William.
Langley Research Center.

January 1973

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

Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory /

Perry, Boyd.
Greene, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

Wind-tunnel investigation of effects of variations in Reynolds number and leading-edge treatment on the aerodynamic characteristics of an externally blown jet-flap configuration /

Parlett, Lysle P.
Megrail, James L.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 8.Mode of access: Internet

A wind-tunnel investigation of the wake near the trailing edge of a deflected externally blown flap /

Johnson, William G. (William Garland), 1944-
Kardas, Gerald E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Chiefly graphs.Cover title.Bibliography: p. 10.Mode of access: I...

Low-speed wind-tunnel investigation of a four-engine upper surface blown model having a swept wing and rectangular and D-shaped exhaust nozzles /

Sleeman, William C.
Hohlweg, William C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18).Mode of ...

Low-speed wind-tunnel investigation of a series of twin-keel all-flexible parawings /

Naeseth, Roger L.
Langley Research Center.

January 1970

Prepared at Langley Research Center."October 1970."Cover title.Includes bibliographical references (...

Subsonic wind-tunnel investigation of a twin-engine attack airplane model having nonmetric powered nacelles /

Lockwood, Vernard E.
Matarazzo, Aniello.
Langley Research Center.

January 1974

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

Wind-tunnel investigation to determine the low-speed yawing stability derivatives of a twin-jet fighter model at high angles of attack /

Coe, Paul L.
Newsom, William A.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Wind-tunnel investigation of internally blown jet-flap STOL airplane model /

Vogler, Raymond D.
United States. National Aeronautics and Space Administration.

January 1976

Issued Nov. 1976.Includes bibliographical references (p. 8).Mode of access: Internet

Wind-tunnel investigation of the flight characteristics of a canard general-aviation airplane configuration /

Satran, Dale R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."October 1986"--Cover.Includes bibliographical references (p. 10...

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...

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

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

An analytical study of the effects of jets located more than one jet diameter above a wing at subsonic speeds /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1974

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

Results of full-scale wind tunnel tests on the H.126 jet flap aircraft /

Aiken, Thomas N.
Cook, Anthony, M.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Bibliography: p. 4.Mode of access: Internet

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 ...

Lowspeed wind-tunnel investigation of a semispan STOL jet transport wing-body with an upper-surface blown jet flap /

Phelps, Arthur R.
Henderson, Robert L.
Letko, William.
Langley Research Center.

January 1973

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

Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory /

Perry, Boyd.
Greene, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

Wind-tunnel investigation of effects of variations in Reynolds number and leading-edge treatment on the aerodynamic characteristics of an externally blown jet-flap configuration /

Parlett, Lysle P.
Megrail, James L.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 8.Mode of access: Internet

A wind-tunnel investigation of the wake near the trailing edge of a deflected externally blown flap /

Johnson, William G. (William Garland), 1944-
Kardas, Gerald E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Chiefly graphs.Cover title.Bibliography: p. 10.Mode of access: I...

Low-speed wind-tunnel investigation of a four-engine upper surface blown model having a swept wing and rectangular and D-shaped exhaust nozzles /

Sleeman, William C.
Hohlweg, William C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18).Mode of ...

Low-speed wind-tunnel investigation of a series of twin-keel all-flexible parawings /

Naeseth, Roger L.
Langley Research Center.

January 1970

Prepared at Langley Research Center."October 1970."Cover title.Includes bibliographical references (...

Subsonic wind-tunnel investigation of a twin-engine attack airplane model having nonmetric powered nacelles /

Lockwood, Vernard E.
Matarazzo, Aniello.
Langley Research Center.

January 1974

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

Wind-tunnel investigation to determine the low-speed yawing stability derivatives of a twin-jet fighter model at high angles of attack /

Coe, Paul L.
Newsom, William A.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Wind-tunnel investigation of internally blown jet-flap STOL airplane model /

Vogler, Raymond D.
United States. National Aeronautics and Space Administration.

January 1976

Issued Nov. 1976.Includes bibliographical references (p. 8).Mode of access: Internet

Wind-tunnel investigation of the flight characteristics of a canard general-aviation airplane configuration /

Satran, Dale R.
Langley Research Center.

January 1986

Prepared at Langley Research Center."October 1986"--Cover.Includes bibliographical references (p. 10...

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...

Pressure measurements of the leading edge of a swept wing at Mach 2.2 /

Sorrells, Russell B.
Langley Research Center.

January 1974

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

An analytical study of the effects of jets located more than one jet diameter above a wing at subsonic speeds /

Putnam, Lawrence E. (Lawrence Elwood)
Langley Research Center.

January 1974

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

Results of full-scale wind tunnel tests on the H.126 jet flap aircraft /

Aiken, Thomas N.
Cook, Anthony, M.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Bibliography: p. 4.Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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