Development and demonstration of a flutter-suppression system using active controls /

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 ...

Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles /

Martin, Dennis J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"November 9, 1951."Includes bibliographical references (p. 12).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...

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...

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....

Flutter suppression using active controls based on the concept of aerodynamic energy [electronic resource] /

Nissim, E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Flutter suppression with dissipated energy reduced to quadratic form for control surfaces.Prepared a...

Control surface spanwise placement in active flutter suppression systems /

Nissim, E.
Burken, John J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"November 1988"--Cover.Includes bibliographical references (p. 11).Mode of access: Internet

A method for obtaining practical flutter-suppression control laws using results of optimal control theory /

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

January 1979

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

Passive control of wing/store flutter /

Reed, Wilmer H.
Foughner, Jerome T.
Cazier, F. W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Eigenspace techniques for active flutter suppression /

Garrard, William L.
Farm, Jerome A.
Liebst, Bradley S. (Bradley Scott)

January 1987

"Prepared for Langley Research Center under Grant NAG1-217.""June 1987"--Cover.Includes bibliographi...

Application of the aerodynamic energy concept to flutter suppression and gust alleviation by use of active controls /

Nissim, E.
Caspi, A., joint author.
Lottati, I., joint author.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 45-46).Mode of access: Internet

Recent advances in aerodynamic energy concept for flutter suppression and gust alleviation using active controls.

Nissim, E.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1977

Sponsored by the National Aeronautics and Space Administration, Washington, D.C.Prepared at NASA Lan...

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...

Automated procedure for design of wing structures to satisfy strength and flutter requirements /

Haftka, Raphael T.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 22-24.Mode of access: Internet

Some effects of tip fins of wing flutter characteristics /

Goetz, Robert C. (Robert Charles), 1937-
Doggett, Robert V.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode ...

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 ...

Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles /

Martin, Dennis J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"November 9, 1951."Includes bibliographical references (p. 12).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...

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...

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....

Flutter suppression using active controls based on the concept of aerodynamic energy [electronic resource] /

Nissim, E.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Flutter suppression with dissipated energy reduced to quadratic form for control surfaces.Prepared a...

Control surface spanwise placement in active flutter suppression systems /

Nissim, E.
Burken, John J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"November 1988"--Cover.Includes bibliographical references (p. 11).Mode of access: Internet

A method for obtaining practical flutter-suppression control laws using results of optimal control theory /

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

January 1979

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

Passive control of wing/store flutter /

Reed, Wilmer H.
Foughner, Jerome T.
Cazier, F. W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Eigenspace techniques for active flutter suppression /

Garrard, William L.
Farm, Jerome A.
Liebst, Bradley S. (Bradley Scott)

January 1987

"Prepared for Langley Research Center under Grant NAG1-217.""June 1987"--Cover.Includes bibliographi...

Application of the aerodynamic energy concept to flutter suppression and gust alleviation by use of active controls /

Nissim, E.
Caspi, A., joint author.
Lottati, I., joint author.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 45-46).Mode of access: Internet

Recent advances in aerodynamic energy concept for flutter suppression and gust alleviation using active controls.

Nissim, E.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1977

Sponsored by the National Aeronautics and Space Administration, Washington, D.C.Prepared at NASA Lan...

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...

Automated procedure for design of wing structures to satisfy strength and flutter requirements /

Haftka, Raphael T.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 22-24.Mode of access: Internet

Some effects of tip fins of wing flutter characteristics /

Goetz, Robert C. (Robert Charles), 1937-
Doggett, Robert V.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11-12).Mode ...

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 ...

Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles /

Martin, Dennis J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"November 9, 1951."Includes bibliographical references (p. 12).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...

Development and demonstration of a flutter-suppression system using active controls /

Abstract

Extracted data

Development and demonstration of a flutter-suppression system using active controls /

Abstract

Extracted data

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