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

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

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

Flutter of a 60©� delta wing (NACA 65A003 airfoil) encountered at supersonic speeds during the flight test of a rocket-propelled model /

Judd, Joseph H.
Lauten, William T.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

NACA Research Memorandum L54D12A."September 25, 1952."Includes bibliographical references (p. 6).Mod...

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

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

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

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

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

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

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

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

Flutter investigation of a true-speed dynamic model with various tip-tank configurations /

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

January 1955

"March 30, 1955."Stores, airplane components; Vibration and flutter; wings and ailerons.Includes bib...

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

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...

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

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

Flutter of a 60©� delta wing (NACA 65A003 airfoil) encountered at supersonic speeds during the flight test of a rocket-propelled model /

Judd, Joseph H.
Lauten, William T.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

NACA Research Memorandum L54D12A."September 25, 1952."Includes bibliographical references (p. 6).Mod...

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

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

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

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

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

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

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

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

Flutter investigation of a true-speed dynamic model with various tip-tank configurations /

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

January 1955

"March 30, 1955."Stores, airplane components; Vibration and flutter; wings and ailerons.Includes bib...

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

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...

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

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

Flutter of a 60©� delta wing (NACA 65A003 airfoil) encountered at supersonic speeds during the flight test of a rocket-propelled model /

Judd, Joseph H.
Lauten, William T.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

NACA Research Memorandum L54D12A."September 25, 1952."Includes bibliographical references (p. 6).Mod...

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

Abstract

Extracted data

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

Abstract

Extracted data

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