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

Aerodynamic performance of flared fan nozzles used as inlets /

Dietrich, Donald A.
Kelm, Gary G., joint author.
Keith, Theo G., joint author.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

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...

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...

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 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...

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

Sandford, M. C. (Maynard C.)
Gray, David L. (David Lewis)
Abel, Irving.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 62-65).Mode ...

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....

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 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 ...

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

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 ...

Gust generator for a supersonic wind tunnel /

Sanders, Bobby W.
Webb, John A.
Bishop, Allan R.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

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...

Theoretical investigation of the subsonic and supersonic flutter characteristics of a swept wing employing a tuned sting-mass flutter suppressor /

Yates, E. Carson.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Stresses and loads.Includes bibliographical references.Mode of access: I...

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...

Aerodynamic performance of flared fan nozzles used as inlets /

Dietrich, Donald A.
Kelm, Gary G., joint author.
Keith, Theo G., joint author.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

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...

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...

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 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...

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

Sandford, M. C. (Maynard C.)
Gray, David L. (David Lewis)
Abel, Irving.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 62-65).Mode ...

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....

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 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 ...

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

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 ...

Gust generator for a supersonic wind tunnel /

Sanders, Bobby W.
Webb, John A.
Bishop, Allan R.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

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...

Theoretical investigation of the subsonic and supersonic flutter characteristics of a swept wing employing a tuned sting-mass flutter suppressor /

Yates, E. Carson.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Stresses and loads.Includes bibliographical references.Mode of access: I...

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...

Aerodynamic performance of flared fan nozzles used as inlets /

Dietrich, Donald A.
Kelm, Gary G., joint author.
Keith, Theo G., joint author.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

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...

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...

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

Abstract

Extracted data

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

Abstract

Extracted data

Related items

Related items