Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow /

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...

Study of lee-side flows over conically cambered delta wings at supersonic speeds /

Wood, Richard M.
Watson, Carolyn B.
Langley Research Center.

January 1987

Prepared at Langley Research Center.Bibliography: v. 1, p. 26.Mode of access: Internet

Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing /

Darden, Christine M.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 9-10.Mode of access: Internet

Low-speed wind-tunnel investigation of flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration /

Coe, Paul L.
Owens, D. B. (Donald Bruce), 1922-
Turner, Steven G. (Steven George)
Langley Research Center.

January 1990

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

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

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 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 ...

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 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 ...

Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model /

Applin, Zachary T.
Gentry, Garl L.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 21.Mode of access: Internet

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).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...

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 ...

Steady-state and transitional aerodynamic characteristics of a wing in simulated heavy rain /

Campbell, Bryan A.
Bezos, Gaudy M.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 60.Mode of access: Internet

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 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...

Study of lee-side flows over conically cambered delta wings at supersonic speeds /

Wood, Richard M.
Watson, Carolyn B.
Langley Research Center.

January 1987

Prepared at Langley Research Center.Bibliography: v. 1, p. 26.Mode of access: Internet

Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing /

Darden, Christine M.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 9-10.Mode of access: Internet

Low-speed wind-tunnel investigation of flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration /

Coe, Paul L.
Owens, D. B. (Donald Bruce), 1922-
Turner, Steven G. (Steven George)
Langley Research Center.

January 1990

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

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

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 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 ...

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 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 ...

Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model /

Applin, Zachary T.
Gentry, Garl L.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 21.Mode of access: Internet

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).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...

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 ...

Steady-state and transitional aerodynamic characteristics of a wing in simulated heavy rain /

Campbell, Bryan A.
Bezos, Gaudy M.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 60.Mode of access: Internet

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 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...

Study of lee-side flows over conically cambered delta wings at supersonic speeds /

Wood, Richard M.
Watson, Carolyn B.
Langley Research Center.

January 1987

Prepared at Langley Research Center.Bibliography: v. 1, p. 26.Mode of access: Internet

Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing /

Darden, Christine M.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 9-10.Mode of access: Internet

Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow /

Abstract

Extracted data

Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow /

Abstract

Extracted data

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