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

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

Hallissy, James B.
Phillips, Pamela S.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 5-6.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

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...

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...

Transonic flutter study of a 50.5 ̊cropped-delta wing with two rearward-mounted nacelles /

Sandford, M. C. (Maynard C.)
Abel, Irving.
Ruhlin, Charles L.
Langley Research Center.

January 1974

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

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 ...

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 ...

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

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:...

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 ...

Flutter analysis and testing of pairs of aerodynamically interfering delta wings /

Chipman, Richard R.
Rauch, Frank J.
Langley Research Center.
Grumman Aerospace Corporation.

January 1973

"Prepared by Grumann Aerospace Corporation ... for Langley Research Center."Cover title.Bibliography...

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 ...

Comparison of analytical and wind-tunnel results for flutter and gust response of a transport wing with active controls /

Abel, Irving.
Newsom, Jerry R.
Perry, Boyd.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject category 39."June 1982"--Cover."Langley Research Center."Includes bibliographical references...

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 investigation of steady-state aerodynamics of a composite-lift VTOL aircraft model /

Winston, Matthew M.
Huston, Robert J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Prepared at Langley Research Center.N69-28097.Cover title.Includes bibliographical references (p. 9)...

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

Hallissy, James B.
Phillips, Pamela S.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 5-6.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

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...

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...

Transonic flutter study of a 50.5 ̊cropped-delta wing with two rearward-mounted nacelles /

Sandford, M. C. (Maynard C.)
Abel, Irving.
Ruhlin, Charles L.
Langley Research Center.

January 1974

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

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 ...

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 ...

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

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:...

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 ...

Flutter analysis and testing of pairs of aerodynamically interfering delta wings /

Chipman, Richard R.
Rauch, Frank J.
Langley Research Center.
Grumman Aerospace Corporation.

January 1973

"Prepared by Grumann Aerospace Corporation ... for Langley Research Center."Cover title.Bibliography...

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 ...

Comparison of analytical and wind-tunnel results for flutter and gust response of a transport wing with active controls /

Abel, Irving.
Newsom, Jerry R.
Perry, Boyd.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject category 39."June 1982"--Cover."Langley Research Center."Includes bibliographical references...

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 investigation of steady-state aerodynamics of a composite-lift VTOL aircraft model /

Winston, Matthew M.
Huston, Robert J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1969

Prepared at Langley Research Center.N69-28097.Cover title.Includes bibliographical references (p. 9)...

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

Hallissy, James B.
Phillips, Pamela S.
Langley Research Center.

January 1989

Research done at Langley Research Center.Bibliography: p. 5-6.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

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

Abstract

Extracted data

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

Abstract

Extracted data

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