An analytical study of the longitudinal response of airplanes to positive wind shear /

Low-altitude wind measurements from wide-body jet transports /

Dunham, R. Earl.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"October 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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:...

Optimality study of a gust alleviation system for light wing-loading STOL aircraft /

Komoda, Masaki.
Ames Research Center.

January 1976

Cover title.Includes bibliographical references (p. 39-40).Mode of access: Internet

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

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 ...

Statistics of some atmospheric turbulence records relevant to aircraft response calculations /

Mark, William D.
Fischer, Raymond W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject Category 05."September 1981"--Cover.Includes bibliographical references.Mode of access: Inte...

Characterization, parameter estimation, and aircraft response statistics of atmospheric turbulence /

Mark, William D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject Category 05."September 1981"--Cover.Includes bibliographical references.Mode of access: Inte...

An analytical study of aircraft lateral-directional handling qualities using pilot models /

Adams, James J.
Moore, Frederick L. (Frederick Lyle), 1943-
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-24).Mode ...

Pilot-aircraft system response to wind shear /

Turkel, Barry S.
Frost, Walter, 1935-
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"Contract NAS8-33458."Nov. 1980.Includes bibliographical references.Mode of access: Internet

Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results /

Redd, L. Tracy.
Wynne, Eleanor C.
Hanson, Perry W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1979

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

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...

Survey on effect of surface winds on aircraft design and operation and recommendations for needed wind research /

Houbolt, John C.
United States. National Aeronautics and Space Administration.

January 1973

"December 1973."Includes bibliographical references (p. 42-63).Mode of access: Internet

Experimental and predicted longitudinal response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet /

Cole, Henry A. Jr.
Holleman, Euclid C., joint author.
Brown, Stuart C., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "November 26, 1954."Includes bibliographical references: p. 32-33.Mode of access: In...

Flight investigation of some effects of a vane-controlled gust-alleviation system on the wing and tail loads fo a transport airplane /

Schott, Russell L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; St...

Wind-tunnel investigation of the effects of wing bodies, fences, flaps, and fuselage addition on the wing buffet response of a transonic-transport model /

Cornette, Elden S.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Low-altitude wind measurements from wide-body jet transports /

Dunham, R. Earl.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"October 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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:...

Optimality study of a gust alleviation system for light wing-loading STOL aircraft /

Komoda, Masaki.
Ames Research Center.

January 1976

Cover title.Includes bibliographical references (p. 39-40).Mode of access: Internet

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

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 ...

Statistics of some atmospheric turbulence records relevant to aircraft response calculations /

Mark, William D.
Fischer, Raymond W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject Category 05."September 1981"--Cover.Includes bibliographical references.Mode of access: Inte...

Characterization, parameter estimation, and aircraft response statistics of atmospheric turbulence /

Mark, William D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject Category 05."September 1981"--Cover.Includes bibliographical references.Mode of access: Inte...

An analytical study of aircraft lateral-directional handling qualities using pilot models /

Adams, James J.
Moore, Frederick L. (Frederick Lyle), 1943-
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-24).Mode ...

Pilot-aircraft system response to wind shear /

Turkel, Barry S.
Frost, Walter, 1935-
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

"Contract NAS8-33458."Nov. 1980.Includes bibliographical references.Mode of access: Internet

Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results /

Redd, L. Tracy.
Wynne, Eleanor C.
Hanson, Perry W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1979

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

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...

Survey on effect of surface winds on aircraft design and operation and recommendations for needed wind research /

Houbolt, John C.
United States. National Aeronautics and Space Administration.

January 1973

"December 1973."Includes bibliographical references (p. 42-63).Mode of access: Internet

Experimental and predicted longitudinal response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet /

Cole, Henry A. Jr.
Holleman, Euclid C., joint author.
Brown, Stuart C., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "November 26, 1954."Includes bibliographical references: p. 32-33.Mode of access: In...

Flight investigation of some effects of a vane-controlled gust-alleviation system on the wing and tail loads fo a transport airplane /

Schott, Russell L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; St...

Wind-tunnel investigation of the effects of wing bodies, fences, flaps, and fuselage addition on the wing buffet response of a transonic-transport model /

Cornette, Elden S.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stresses and loads.Includes bibliographical referen...

Low-altitude wind measurements from wide-body jet transports /

Dunham, R. Earl.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"October 1982"--Cover.Includes bibliographical references.Mode of access: Internet

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:...

Optimality study of a gust alleviation system for light wing-loading STOL aircraft /

Komoda, Masaki.
Ames Research Center.

January 1976

Cover title.Includes bibliographical references (p. 39-40).Mode of access: Internet

An analytical study of the longitudinal response of airplanes to positive wind shear /

Abstract

Extracted data

An analytical study of the longitudinal response of airplanes to positive wind shear /

Abstract

Extracted data

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