Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles /

Investigation toward simplification of missile control systems /

Curfman, Howard J.
Crane, Harold L.
Strass, H. Kurt.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1953

"November 12, 1953."Includes bibliographical references (p. 7).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 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

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

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

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

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

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...

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

Automated preliminary design of simplified wing structures to satisfy strength and flutter requirements /

Stroud, W. Jefferson.
Stein, Manuel.
Dexter, Cornelia B.
United States. National Aeronautics and Space Administration.

January 1971

"December 1971."Cover title.Includes bibliographical references (p. 136-137).Mode of access: Interne...

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

Rocket-powered flight test of a roll-stabilized supersonic missile configuration /

Gardiner, Robert A.
Zarovsky, Jacob.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"January 12, 1950."Includes bibliographical references (p. 12).Mode of access: Internet

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 ...

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

Investigation toward simplification of missile control systems /

Curfman, Howard J.
Crane, Harold L.
Strass, H. Kurt.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1953

"November 12, 1953."Includes bibliographical references (p. 7).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 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

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

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

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

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

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...

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

Automated preliminary design of simplified wing structures to satisfy strength and flutter requirements /

Stroud, W. Jefferson.
Stein, Manuel.
Dexter, Cornelia B.
United States. National Aeronautics and Space Administration.

January 1971

"December 1971."Cover title.Includes bibliographical references (p. 136-137).Mode of access: Interne...

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

Rocket-powered flight test of a roll-stabilized supersonic missile configuration /

Gardiner, Robert A.
Zarovsky, Jacob.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"January 12, 1950."Includes bibliographical references (p. 12).Mode of access: Internet

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 ...

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

Investigation toward simplification of missile control systems /

Curfman, Howard J.
Crane, Harold L.
Strass, H. Kurt.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1953

"November 12, 1953."Includes bibliographical references (p. 7).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 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

Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles /

Abstract

Extracted data

Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles /

Abstract

Extracted data

Related items

Related items