High-angle-of-attack stability characteristics of a three-surface fighter configuration /

Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage /

Dollyhigh, Samuel M.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ...

Low-speed wind-tunnel study of the high-angle-of-attack stability and control characteristics of a cranked-arrow-wing fighter configuration /

Grafton, Sue B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 08.Distributed to depository libraries in microfiche."May 1984"--Cover.Includes bib...

Maneuver and buffet characteristics of fighter aircraft /

Ray, Edward J.
Carmichael, Julian G.
McKinney, Linwood W.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16.Mode of access: Internet

Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45?/

Henderson, William P.
Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"September 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access...

Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47⁰ /

Mann, Michael J.
Fox, Charles H.
Huffman, Jarrett K.
Langley Research Center.

January 1987

Prepared at Langley Research Center."September 1987"--Cover.Includes bibliographical references (p. ...

Hypersonic longitudinal trim, stability, and control characteristics of a delta-wing configuration at high angles of attack /

Close, William H.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Experimental study of wing leading-edge devices for improved maneuver performance of a supercritical maneuvering fighter configuration /

Mann, Michael J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"March 1983"--Cover.Includes bibliographical references.Mode of access: Internet

Calculation of aerodynamic characteristics of airplane configurations at high angles of attack /

Tseng, Jing-Biau.
Lan, C. Edward (Chun-Tau Edward), 1935-
Langley Research Center.

January 1988

"October 1988"--Cover."Prepared for Langley Research Center under Grant NAG1-635."Includes bibliogra...

An analysis of the delta-wing hypersonic stability and control behavior at angles of attack between 30 degrees and 90 degrees

Fetterman, David E.
Neal, Luther.
United States. National Aeronautics and Space Administration.

Cover title."March 1963."Includes bibliographical references.Mode of access: Internet

Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces /

Robinson, Ross B.
Foster, Gerald V.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Aerodynamic characteristics of three axismmetric low-fitness-ratio reentry shapes at Mach 6.9 /

Penland, Jim A.
Bernot, Peter T.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack /

Satran, Dale R.
Anglin, Ernie L.
Gilbert, William P.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 9-10)....

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01 /

Foster, Gerald V.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 6).Mode of access: Inte...

Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser /

Banks, Daniel W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"October 1988"--Cover.Includes bibliographical references (p. 11).Mode of access: Internet

Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep /

Luoma, Arvo A.
Alford, William J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 12-13).Mode of access: Internet

Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage /

Dollyhigh, Samuel M.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ...

Low-speed wind-tunnel study of the high-angle-of-attack stability and control characteristics of a cranked-arrow-wing fighter configuration /

Grafton, Sue B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 08.Distributed to depository libraries in microfiche."May 1984"--Cover.Includes bib...

Maneuver and buffet characteristics of fighter aircraft /

Ray, Edward J.
Carmichael, Julian G.
McKinney, Linwood W.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16.Mode of access: Internet

Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45?/

Henderson, William P.
Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"September 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access...

Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47⁰ /

Mann, Michael J.
Fox, Charles H.
Huffman, Jarrett K.
Langley Research Center.

January 1987

Prepared at Langley Research Center."September 1987"--Cover.Includes bibliographical references (p. ...

Hypersonic longitudinal trim, stability, and control characteristics of a delta-wing configuration at high angles of attack /

Close, William H.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Experimental study of wing leading-edge devices for improved maneuver performance of a supercritical maneuvering fighter configuration /

Mann, Michael J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"March 1983"--Cover.Includes bibliographical references.Mode of access: Internet

Calculation of aerodynamic characteristics of airplane configurations at high angles of attack /

Tseng, Jing-Biau.
Lan, C. Edward (Chun-Tau Edward), 1935-
Langley Research Center.

January 1988

"October 1988"--Cover."Prepared for Langley Research Center under Grant NAG1-635."Includes bibliogra...

An analysis of the delta-wing hypersonic stability and control behavior at angles of attack between 30 degrees and 90 degrees

Fetterman, David E.
Neal, Luther.
United States. National Aeronautics and Space Administration.

Cover title."March 1963."Includes bibliographical references.Mode of access: Internet

Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces /

Robinson, Ross B.
Foster, Gerald V.
Langley Research Center.

January 1961

"April 1961."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Aerodynamic characteristics of three axismmetric low-fitness-ratio reentry shapes at Mach 6.9 /

Penland, Jim A.
Bernot, Peter T.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack /

Satran, Dale R.
Anglin, Ernie L.
Gilbert, William P.
Langley Research Center.

January 1985

Prepared at Langley Research Center."May 1985"--Cover.Includes bibliographical references (p. 9-10)....

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01 /

Foster, Gerald V.
Langley Research Center.

January 1959

"November 1959"--Cover.Caption title.Includes bibliographical references (p. 6).Mode of access: Inte...

Aerodynamics in ground effect and predicted landing ground roll of a fighter configuration with a secondary-nozzle thrust reverser /

Banks, Daniel W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"October 1988"--Cover.Includes bibliographical references (p. 11).Mode of access: Internet

Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep /

Luoma, Arvo A.
Alford, William J.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 12-13).Mode of access: Internet

Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage /

Dollyhigh, Samuel M.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ...

Low-speed wind-tunnel study of the high-angle-of-attack stability and control characteristics of a cranked-arrow-wing fighter configuration /

Grafton, Sue B.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 08.Distributed to depository libraries in microfiche."May 1984"--Cover.Includes bib...

Maneuver and buffet characteristics of fighter aircraft /

Ray, Edward J.
Carmichael, Julian G.
McKinney, Linwood W.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16.Mode of access: Internet

High-angle-of-attack stability characteristics of a three-surface fighter configuration /

Abstract

Extracted data

High-angle-of-attack stability characteristics of a three-surface fighter configuration /

Abstract

Extracted data

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