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

An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics /

Doggett, Robert V.
Morgan, Homer G.
Rainey, A. Gerald.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Preliminary results of supersonic-jet tests of simplified wing structures /

Heldenfels, Richard R.
Rosecrans, Richard.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 8, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

A compilation of experimental flutter information /

Cunningham, H. J.
Brown Harvey H.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"January 11, 1954."Includes bibliographical references (p. 6-11).Mode of access: Internet

Investigation of wing flutter at transonic speeds for six systematically varied wing plan forms /

Jones, George W.
DuBose, Hugh C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"August 13, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

Flutter investigation of two thin, low-aspect-ratio, swept, solid, metal wings in the transonic range by use of free-falling body /

Lauten, W. T.
Sylvester, Maurice A.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"February 26, 1952."Includes bibliographical references (p. 7).Mode of access: Internet

Flutter characteristics of swept wings at transonic speeds /

Loftin, Laurence K.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"July 6, 1955."Includes bibliographical references (p. 10).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

Some experimental studies of panel flutter at Mach number 1.3 /

Sylvester, Maurice A.
Baker, John E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"December 1, 1952."Includes bibliographical references (p. 11).Mode of access: Internet

Transonic flutter investigation of two 50©� semispan modified-delta wings with tip ailerons /

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

January 1958

"February 17, 1958."Includes bibliographical references (p. 6).Mode of access: Internet

Transonic flight tests to determine the effect of thickness ratio and plan-form modification on the zero-lift drag of a 45©� sweptback wing /

Pepper, William B.
Hoffman, Sherwood.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"August 12, 1952."Includes bibliographical references (p. 9).Mode of access: Internet

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

Transonic flutter tests of a highly swept arrow wing with and without simulated trailing-edge-mounted engine masses /

Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Stresses and loads.Includes bibliographical references.Mode of access: Inte...

Transonic and supersonic flutter trend investigation of a variable-sweep wing /

Stonesifer, John C.
Goetz, Robert C.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

An experimental transonic investigation of a 45©� sweptback wing-body combination with several types of body indentation with theoretical comparisons included /

Carmel, Melvin M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 19,1954."Includes bibliographical references (p. 11).Mode of access: Internet

Use of experimental steady-flow aerodynamic parameters in the calculation of flutter characteristics for finite-span swept or unswept wings at subsonic, transonic, and supersonic speed /

Yates, E. Carson (Edward Carson), 1926-
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 19-20).Mode of access: Internet

An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics /

Doggett, Robert V.
Morgan, Homer G.
Rainey, A. Gerald.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Preliminary results of supersonic-jet tests of simplified wing structures /

Heldenfels, Richard R.
Rosecrans, Richard.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 8, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

A compilation of experimental flutter information /

Cunningham, H. J.
Brown Harvey H.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"January 11, 1954."Includes bibliographical references (p. 6-11).Mode of access: Internet

Investigation of wing flutter at transonic speeds for six systematically varied wing plan forms /

Jones, George W.
DuBose, Hugh C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"August 13, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

Flutter investigation of two thin, low-aspect-ratio, swept, solid, metal wings in the transonic range by use of free-falling body /

Lauten, W. T.
Sylvester, Maurice A.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"February 26, 1952."Includes bibliographical references (p. 7).Mode of access: Internet

Flutter characteristics of swept wings at transonic speeds /

Loftin, Laurence K.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"July 6, 1955."Includes bibliographical references (p. 10).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

Some experimental studies of panel flutter at Mach number 1.3 /

Sylvester, Maurice A.
Baker, John E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"December 1, 1952."Includes bibliographical references (p. 11).Mode of access: Internet

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

January 1958

"February 17, 1958."Includes bibliographical references (p. 6).Mode of access: Internet

Transonic flight tests to determine the effect of thickness ratio and plan-form modification on the zero-lift drag of a 45©� sweptback wing /

Pepper, William B.
Hoffman, Sherwood.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"August 12, 1952."Includes bibliographical references (p. 9).Mode of access: Internet

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

Transonic flutter tests of a highly swept arrow wing with and without simulated trailing-edge-mounted engine masses /

Walberg, Gerald D.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Stresses and loads.Includes bibliographical references.Mode of access: Inte...

Transonic and supersonic flutter trend investigation of a variable-sweep wing /

Stonesifer, John C.
Goetz, Robert C.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

An experimental transonic investigation of a 45©� sweptback wing-body combination with several types of body indentation with theoretical comparisons included /

Carmel, Melvin M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"November 19,1954."Includes bibliographical references (p. 11).Mode of access: Internet

Use of experimental steady-flow aerodynamic parameters in the calculation of flutter characteristics for finite-span swept or unswept wings at subsonic, transonic, and supersonic speed /

Yates, E. Carson (Edward Carson), 1926-
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 19-20).Mode of access: Internet

An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics /

Doggett, Robert V.
Morgan, Homer G.
Rainey, A. Gerald.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Preliminary results of supersonic-jet tests of simplified wing structures /

Heldenfels, Richard R.
Rosecrans, Richard.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 8, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

A compilation of experimental flutter information /

Cunningham, H. J.
Brown Harvey H.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"January 11, 1954."Includes bibliographical references (p. 6-11).Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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