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

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 small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ref...

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

Satran, Dale R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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

Large-scale wind-tunnel tests of an airplane model with two propellers and rotaing cylinder flaps /

Weiberg, James A.
Gamse, Berl.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 9).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 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 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 ...

Large-scale wind-tunnel tests of a deflected slipstream STOL model with wings of various aspect ratios /

Page, V. Robert.
Deckert, W. H. (Wallace H.)
Dickinson, Stanley O.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 7).Mode of access: Internet

Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle /

Johnson, Joseph L.
Hassell, James L.
United States. National Aeronautics and Space Administration.

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

A wind-tunnel investigation of a 4-foot-diameter ducted fan mounted on the tip of a semispan wing /

Yaggy, Paul F.
Mort, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stability and control;Includes bibli...

Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.08 chord below wing /

Fink, Marvin P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 12).Mode of access: Internet

Large-scale wind-tunnel investigation of an airplane model with a tilt wing of aspect ratio 8.4, and four propellers, in the presence of a ground plane /

Dickinson, Stanley O.
Deckert, W. H. (Wallace H.)
Page, V. Robert.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 7).Mode of access: Internet

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...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

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 small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ref...

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

Satran, Dale R.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

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

Large-scale wind-tunnel tests of an airplane model with two propellers and rotaing cylinder flaps /

Weiberg, James A.
Gamse, Berl.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 9).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 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 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 ...

Large-scale wind-tunnel tests of a deflected slipstream STOL model with wings of various aspect ratios /

Page, V. Robert.
Deckert, W. H. (Wallace H.)
Dickinson, Stanley O.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 7).Mode of access: Internet

Full-scale wind-tunnel investigation of a flexible-wing manned test vehicle /

Johnson, Joseph L.
Hassell, James L.
United States. National Aeronautics and Space Administration.

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

A wind-tunnel investigation of a 4-foot-diameter ducted fan mounted on the tip of a semispan wing /

Yaggy, Paul F.
Mort, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stability and control;Includes bibli...

Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.08 chord below wing /

Fink, Marvin P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 12).Mode of access: Internet

Large-scale wind-tunnel investigation of an airplane model with a tilt wing of aspect ratio 8.4, and four propellers, in the presence of a ground plane /

Dickinson, Stanley O.
Deckert, W. H. (Wallace H.)
Page, V. Robert.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 7).Mode of access: Internet

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...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

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 small-scale model of an aerial vehicle supported by tilting ducted fans /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."August 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ref...

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

Abstract

Extracted data

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

Abstract

Extracted data

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