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

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...

Dynamic and static wind-tunnel tests of a flow-direction vane /

Richardson, Norman R.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."April 1971."Cover title.Includes bibliographical references (p....

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...

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:...

Application of two design methods for active flutter suppression and wind-tunnel test results /

Newsom, Jerry R.
Dunn, H. J., 1947-
Abel, Irving.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject Category 39."May 1980"--Cover."Langley Research Center."Includes bibliographical references....

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 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...

Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model /

Ruhlin, Charles L.
Nagaraja, K. S.
Bhatia, Kumar G. (Kumar Gobindram), 1941-
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 2...

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 interference factors for high-lift wings in closed wind tunnels /

Joppa, Robert G. (Robert Glenn)
Langley Research Center.
University of Washington.

"February 1973.""Prepared by University of Washington ... for Langley Research Center."Cover title.I...

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 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:...

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 ...

Evaluation of flow quality in two large NASA wind tunnels at transonic speeds /

Harvey, Bill.
Owen, F. Kevin.
Stainback, P. Calvin.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 34."December 1980"--Cover."Langley Research Center."Includes bibliographical refere...

Application of model control to wing-flutter suppression /

Ostroff, Aaron J.
Pines, Samuel.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"May 1982"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

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...

Dynamic and static wind-tunnel tests of a flow-direction vane /

Richardson, Norman R.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."April 1971."Cover title.Includes bibliographical references (p....

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...

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:...

Application of two design methods for active flutter suppression and wind-tunnel test results /

Newsom, Jerry R.
Dunn, H. J., 1947-
Abel, Irving.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

Subject Category 39."May 1980"--Cover."Langley Research Center."Includes bibliographical references....

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 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...

Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model /

Ruhlin, Charles L.
Nagaraja, K. S.
Bhatia, Kumar G. (Kumar Gobindram), 1941-
Langley Research Center.

January 1986

Prepared at Langley Research Center."December 1986"--Cover.Includes bibliographical references (p. 2...

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 interference factors for high-lift wings in closed wind tunnels /

Joppa, Robert G. (Robert Glenn)
Langley Research Center.
University of Washington.

"February 1973.""Prepared by University of Washington ... for Langley Research Center."Cover title.I...

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 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:...

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 ...

Evaluation of flow quality in two large NASA wind tunnels at transonic speeds /

Harvey, Bill.
Owen, F. Kevin.
Stainback, P. Calvin.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 34."December 1980"--Cover."Langley Research Center."Includes bibliographical refere...

Application of model control to wing-flutter suppression /

Ostroff, Aaron J.
Pines, Samuel.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"May 1982"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

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...

Dynamic and static wind-tunnel tests of a flow-direction vane /

Richardson, Norman R.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Prepared at Langley Research Center."April 1971."Cover title.Includes bibliographical references (p....

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...

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

Abstract

Extracted data

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

Abstract

Extracted data

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