Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes /

Wind-tunnel investigation of the validity of a sonic-boom-minimization concept /

Mack, Robert J.
Darden, Christine M.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""October 1979"--Cover.Includes bibliographical references.Mode of access: ...

Low-speed wind-tunnel investigation of a reflection plane wing equipped with partial-span jet-augmented flaps /

Otis, James H.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Stability and control.Includes bibliographical references.Mode of a...

Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft /

White, E. Richard.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Kentron International.
Langley Research Center.

January 1982

"November 1982"--Cover."Kentron International, Inc."Includes bibliographical references.Mode of acce...

Wind-tunnel experiments on divergence of forward-swept wings /

Ricketts, Rodney H.
Doggett, Robert V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 05."August 1980"--Cover."Langley Research Center."Includes bibliographical referenc...

Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section /

McGhee, Robert J.
Beasley, William D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

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...

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 ...

Wind-tunnel study to explore the use of slot spoilers to modulate the flap-induced lift of a wing /

Stickle, Joseph W.
Henry, Robert C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 5).Mode of access: Internet

Wind tunnel investigation of an all flush orifice air data system for a large subsonic aircraft /

Larson, Terry J.
Siemers, Paul M.
Flechner, Stuart G.
Langley Research Center.
Hugh L. Dryden Flight Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"May 1980"--Cover."Langley Research Center.""Dryden Flight Research Center."Includes bibliographical...

Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack /

Satran, Dale R.
Anglin, Ernie L.
Gilbert, William P.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 9-10)....

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 (...

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 ...

Flight investigation of the effects of an outboard wing-leading-edge modification on stall/spin characteristics of a low-wing, single-engine, T-tail light airplane /

Stough, H. Paul.
Patton, James M., Jr.
DiCarlo, Daniel J.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Aeroacoustic wind-tunnel tests of a light twin-boom general aviation airplane with free or shrouded-pusher propellers /

McLemore, H. Clyde.
Pegg, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"April 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Wind-tunnel study of deflected-elevator flutter encountered on a T-Tail airplane /

Sandford, Maynard C.
Ruhlin, Charles L.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Prepared by Langley Research Center.N 69-16211.Includes bibliographical references (p. 13).Mode of a...

Wind-tunnel investigation of the validity of a sonic-boom-minimization concept /

Mack, Robert J.
Darden, Christine M.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""October 1979"--Cover.Includes bibliographical references.Mode of access: ...

Low-speed wind-tunnel investigation of a reflection plane wing equipped with partial-span jet-augmented flaps /

Otis, James H.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Stability and control.Includes bibliographical references.Mode of a...

Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft /

White, E. Richard.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Kentron International.
Langley Research Center.

January 1982

"November 1982"--Cover."Kentron International, Inc."Includes bibliographical references.Mode of acce...

Wind-tunnel experiments on divergence of forward-swept wings /

Ricketts, Rodney H.
Doggett, Robert V.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 05."August 1980"--Cover."Langley Research Center."Includes bibliographical referenc...

Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section /

McGhee, Robert J.
Beasley, William D.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

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...

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 ...

Wind-tunnel study to explore the use of slot spoilers to modulate the flap-induced lift of a wing /

Stickle, Joseph W.
Henry, Robert C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 5).Mode of access: Internet

Wind tunnel investigation of an all flush orifice air data system for a large subsonic aircraft /

Larson, Terry J.
Siemers, Paul M.
Flechner, Stuart G.
Langley Research Center.
Hugh L. Dryden Flight Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"May 1980"--Cover."Langley Research Center.""Dryden Flight Research Center."Includes bibliographical...

Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack /

Satran, Dale R.
Anglin, Ernie L.
Gilbert, William P.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 9-10)....

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 (...

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 ...

Flight investigation of the effects of an outboard wing-leading-edge modification on stall/spin characteristics of a low-wing, single-engine, T-tail light airplane /

Stough, H. Paul.
Patton, James M., Jr.
DiCarlo, Daniel J.
Langley Research Center.

January 1987

Prepared at Langley Research Center."July 1987"--Cover.Includes bibliographical references (p. 9).Mo...

Aeroacoustic wind-tunnel tests of a light twin-boom general aviation airplane with free or shrouded-pusher propellers /

McLemore, H. Clyde.
Pegg, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"April 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Wind-tunnel study of deflected-elevator flutter encountered on a T-Tail airplane /

Sandford, Maynard C.
Ruhlin, Charles L.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Prepared by Langley Research Center.N 69-16211.Includes bibliographical references (p. 13).Mode of a...

Wind-tunnel investigation of the validity of a sonic-boom-minimization concept /

Mack, Robert J.
Darden, Christine M.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"Langley Research Center.""October 1979"--Cover.Includes bibliographical references.Mode of access: ...

Low-speed wind-tunnel investigation of a reflection plane wing equipped with partial-span jet-augmented flaps /

Otis, James H.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Stability and control.Includes bibliographical references.Mode of a...

Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft /

White, E. Richard.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Kentron International.
Langley Research Center.

January 1982

"November 1982"--Cover."Kentron International, Inc."Includes bibliographical references.Mode of acce...

Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes /

Abstract

Extracted data

Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes /

Abstract

Extracted data

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