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 /

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...

Results of two experiments on flutter of high-aspect-ratio swept wings in the transonic speed range /

Lauten, William T.
O'Kelly, Burke R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 3, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

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...

Preliminary investigation at low speeds of swept wings in rolling flow /

Feigenbaum, David.
Goodman, Alex.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1947

"May 22, 1947."Includes bibliographical references (p. 12).Mode of access: Internet

Experimental and analytical investigation of flutter of a nonuniform sweptback cantilever wing with two concentrated weights /

Sewall, John L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"December 4, 1951."Includes bibliographical references (p. 17).Mode of access: Internet

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...

An experimental investigation of the effects of Mach number, stabilizer dihedral, and fin torsional stiffness on the transonic flutter characteristics of a tee-tail /

Land, Norman S.
Fox, Annie G.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"October 23, 1957."Includes bibliographical references (p. 8).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...

Effect of structural flexibiligy on aircraft loading.

Engel, S. J., author.
McCarthy, J. F., Jr., 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.
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...

Aerodynamic characteristics of several cranked leading-edge wing-body combinations at Mach numbers from 0.4 to 2.94 /

Hopkins, Edward J.
Carmichael, Ralph L.
Hicks, Raymond M.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1967

"October 1967."Includes bibliographical references (p.21).Mode of access: Internet

Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45©� sweptback wing at high subsonic speeds /

Wiggins, James W.
Kuhn, Richard E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1954

"November 6, 1953."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

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.

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.

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...

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...

Results of two experiments on flutter of high-aspect-ratio swept wings in the transonic speed range /

Lauten, William T.
O'Kelly, Burke R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 3, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

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...

Preliminary investigation at low speeds of swept wings in rolling flow /

Feigenbaum, David.
Goodman, Alex.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1947

"May 22, 1947."Includes bibliographical references (p. 12).Mode of access: Internet

Experimental and analytical investigation of flutter of a nonuniform sweptback cantilever wing with two concentrated weights /

Sewall, John L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1951

"December 4, 1951."Includes bibliographical references (p. 17).Mode of access: Internet

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...

An experimental investigation of the effects of Mach number, stabilizer dihedral, and fin torsional stiffness on the transonic flutter characteristics of a tee-tail /

Land, Norman S.
Fox, Annie G.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"October 23, 1957."Includes bibliographical references (p. 8).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...

Effect of structural flexibiligy on aircraft loading.

Engel, S. J., author.
McCarthy, J. F., Jr., 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.
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...

Aerodynamic characteristics of several cranked leading-edge wing-body combinations at Mach numbers from 0.4 to 2.94 /

Hopkins, Edward J.
Carmichael, Ralph L.
Hicks, Raymond M.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1967

"October 1967."Includes bibliographical references (p.21).Mode of access: Internet

Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45©� sweptback wing at high subsonic speeds /

Wiggins, James W.
Kuhn, Richard E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1954

"November 6, 1953."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

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.

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.

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...

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...

Results of two experiments on flutter of high-aspect-ratio swept wings in the transonic speed range /

Lauten, William T.
O'Kelly, Burke R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 3, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

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...

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 /

Abstract

Extracted data

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 /

Abstract

Extracted data

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