Effect of structural flexibiligy on aircraft loading.

Some modifications of the common theory of flexure with special reference to the design of wood beams used in air craft /

Trayer, George W. (George William), 1888-1976.

January 1922

Typescript.Thesis (C.E.)--University of Wisconsin--Madison, 1922.Mode of access: Internet

Effects of angle of attack and thickness ratio on the flutter of a rigid unswept diamond-airfoil-section wing at a Mach number of 10.0 /

Young, Lou S.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Stresses and loads.Includes bibliographical references.Mode of access: Int...

Fatigue investigation of full-scale transport-airplane wings tests with constant-amplitude and variable amplitude loading schedules/

Foster, Lee R.
Whlaey, Richard E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Stresses and loads.Includes bibliographical references.Mode of access: In...

Effect of structural flexibiligy on aircraft loading.

Foss, K. A., author.
Pian, Theodore H. H., 1919-2009, author.
Sternlight D., author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Effect of structural flexibiligy on aircraft loading.

Pian, Theodore H. H., 1919-2009, author.
Winter, P. H., author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Effect of structural flexibiligy on aircraft loading.

Pian, Theodore H. H., 1919-2009, author.
Lin, Hua, author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Effect of structural flexibiligy on aircraft loading.

Codik, A., author.
Pian, Theodore H. H., 1919-2009, author.
Lin, Hua, author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Effect of structural flexibiligy on aircraft loading.

Carta, F. O. (Franklin O.), author.
Lin, Hua, author.
Pian, Theodore H. H., 1919-2009, author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Effect of structural flexibiligy on aircraft loading.

McCarthy, J. F., Jr., author.
Kirsch, A. A., author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Effect of structural flexibiligy on aircraft loading.

Lin, Hua, author.
Pian, Theodore H. H., 1919-2009, author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Effect of structural flexibiligy on aircraft loading.

Foss, K. A., author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Experimental determination of effect of structural rigidity on rolling effectiveness of some straight and swept wings at Mach numbers from 0.7 to 1.7 /

Strass, H. Kurt.
Purser, Paul E.
Fields, E. M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"October 4, 1950."Includes bibliographical references (p. 11).Mode of access: Internet

Investigation of the fatigue strength of a full-scale airplane wing structures /

Fearnow, Dwight O.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"July 13, 1951."Includes bibliographical references (p. 12).Mode of access: Internet

Effect of structural flexibility on the design of vibration-isolating mounts for aircraft engines /

Phillips, William H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1984

Subject category 39."February 1984"--Cover.Distributed to depository libraries in microfiche.Include...

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...

Some modifications of the common theory of flexure with special reference to the design of wood beams used in air craft /

Trayer, George W. (George William), 1888-1976.

January 1922

Typescript.Thesis (C.E.)--University of Wisconsin--Madison, 1922.Mode of access: Internet

Effects of angle of attack and thickness ratio on the flutter of a rigid unswept diamond-airfoil-section wing at a Mach number of 10.0 /

Young, Lou S.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Stresses and loads.Includes bibliographical references.Mode of access: Int...

Fatigue investigation of full-scale transport-airplane wings tests with constant-amplitude and variable amplitude loading schedules/

Foster, Lee R.
Whlaey, Richard E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Stresses and loads.Includes bibliographical references.Mode of access: In...

Effect of structural flexibiligy on aircraft loading.

Foss, K. A., author.
Pian, Theodore H. H., 1919-2009, author.
Sternlight D., author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Effect of structural flexibiligy on aircraft loading.

Pian, Theodore H. H., 1919-2009, author.
Winter, P. H., author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Effect of structural flexibiligy on aircraft loading.

Pian, Theodore H. H., 1919-2009, author.
Lin, Hua, author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Effect of structural flexibiligy on aircraft loading.

Codik, A., author.
Pian, Theodore H. H., 1919-2009, author.
Lin, Hua, author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Effect of structural flexibiligy on aircraft loading.

Carta, F. O. (Franklin O.), author.
Lin, Hua, author.
Pian, Theodore H. H., 1919-2009, author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Effect of structural flexibiligy on aircraft loading.

McCarthy, J. F., Jr., author.
Kirsch, A. A., author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Effect of structural flexibiligy on aircraft loading.

Lin, Hua, author.
Pian, Theodore H. H., 1919-2009, author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Effect of structural flexibiligy on aircraft loading.

Foss, K. A., author.
Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, sponsor.
Wright Air Development Center, issuing body.

Report prepared by Aero-Elastic and Structures Research Laboratory, Massachusetts Institute of Techn...

Experimental determination of effect of structural rigidity on rolling effectiveness of some straight and swept wings at Mach numbers from 0.7 to 1.7 /

Strass, H. Kurt.
Purser, Paul E.
Fields, E. M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"October 4, 1950."Includes bibliographical references (p. 11).Mode of access: Internet

Investigation of the fatigue strength of a full-scale airplane wing structures /

Fearnow, Dwight O.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"July 13, 1951."Includes bibliographical references (p. 12).Mode of access: Internet

Effect of structural flexibility on the design of vibration-isolating mounts for aircraft engines /

Phillips, William H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1984

Subject category 39."February 1984"--Cover.Distributed to depository libraries in microfiche.Include...

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...

Some modifications of the common theory of flexure with special reference to the design of wood beams used in air craft /

Trayer, George W. (George William), 1888-1976.

January 1922

Typescript.Thesis (C.E.)--University of Wisconsin--Madison, 1922.Mode of access: Internet

Effects of angle of attack and thickness ratio on the flutter of a rigid unswept diamond-airfoil-section wing at a Mach number of 10.0 /

Young, Lou S.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Stresses and loads.Includes bibliographical references.Mode of access: Int...

Fatigue investigation of full-scale transport-airplane wings tests with constant-amplitude and variable amplitude loading schedules/

Foster, Lee R.
Whlaey, Richard E.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Stresses and loads.Includes bibliographical references.Mode of access: In...

Effect of structural flexibiligy on aircraft loading.

Abstract

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Effect of structural flexibiligy on aircraft loading.

Abstract

Extracted data

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