Wind-tunnel investigation of an externally blown flap STOL transport model including an investigation of wall effects /

Large-scale wind-tunnel tests of inverting flaps on a STOL utility aircraft model /

Feistel, Terrell W.
Morelli, Joseph P.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"June 1980"--Cover."Aeromechanics Laboratory, AVRADCOM Research and Technology Laboratories, Ames Re...

Test sections for small theoretical wind-tunnel-boundary interference on V/STOL models /

Wright, Ray H.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Prepared at Langley Research Center.N68 31592.Includes bibliographical references (p. 84-84).Mode of...

Wind-tunnel investigation of an STOL aircraft configuration equipped with an external-flow jet flap /

Parlett, Lysle P.
Shivers, James P.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Wind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with ...

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 ...

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...

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

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

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 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 ...

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 ...

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 ...

Free-flight investigation of the stability and control characteristics of a STOL model with an externally blown jet flap /

Parlett, Lysle P.
Phelps, Arthur E.
Emerling, Sandy J. (Sandy James)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18-20).Mode ...

Effect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL model /

Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Low-speed wind-tunnel investigation of span load alteration, forward-located spoilers, and splines as trailing-vortex-hazard alleviation devices on a transport aircraft model /

Croom, Delwin R.
Dunham, R. Earl.
Langley Research Center.

January 1975

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

Low-speed upwash interference on a transport model in a rectangular slotted-wall wind tunnel /

Mann, Michael J.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Large-scale wind-tunnel tests of inverting flaps on a STOL utility aircraft model /

Feistel, Terrell W.
Morelli, Joseph P.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"June 1980"--Cover."Aeromechanics Laboratory, AVRADCOM Research and Technology Laboratories, Ames Re...

Test sections for small theoretical wind-tunnel-boundary interference on V/STOL models /

Wright, Ray H.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Prepared at Langley Research Center.N68 31592.Includes bibliographical references (p. 84-84).Mode of...

Wind-tunnel investigation of an STOL aircraft configuration equipped with an external-flow jet flap /

Parlett, Lysle P.
Shivers, James P.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Wind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with ...

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 ...

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...

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

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

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 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 ...

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 ...

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 ...

Free-flight investigation of the stability and control characteristics of a STOL model with an externally blown jet flap /

Parlett, Lysle P.
Phelps, Arthur E.
Emerling, Sandy J. (Sandy James)
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18-20).Mode ...

Effect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL model /

Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Low-speed wind-tunnel investigation of span load alteration, forward-located spoilers, and splines as trailing-vortex-hazard alleviation devices on a transport aircraft model /

Croom, Delwin R.
Dunham, R. Earl.
Langley Research Center.

January 1975

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

Low-speed upwash interference on a transport model in a rectangular slotted-wall wind tunnel /

Mann, Michael J.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

Large-scale wind-tunnel tests of inverting flaps on a STOL utility aircraft model /

Feistel, Terrell W.
Morelli, Joseph P.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"June 1980"--Cover."Aeromechanics Laboratory, AVRADCOM Research and Technology Laboratories, Ames Re...

Test sections for small theoretical wind-tunnel-boundary interference on V/STOL models /

Wright, Ray H.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Prepared at Langley Research Center.N68 31592.Includes bibliographical references (p. 84-84).Mode of...

Wind-tunnel investigation of an STOL aircraft configuration equipped with an external-flow jet flap /

Parlett, Lysle P.
Shivers, James P.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Wind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with ...

Wind-tunnel investigation of an externally blown flap STOL transport model including an investigation of wall effects /

Abstract

Extracted data

Wind-tunnel investigation of an externally blown flap STOL transport model including an investigation of wall effects /

Abstract

Extracted data

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