Analysis of the flat-spin characteristics of a twin-jet swept-wing fighter airplane /

Exhaust-nozzle characteristics for a twin-jet variable-wing-sweep fighter airplane model at Mach numbers to 2.2 /

Reubush, David E.
Mercer, Charles E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

The Influence of very heavy fuselage mass loadings and long nose lengths upon oscillations in the spin /

Stone, Ralph W.
Klinar, Walter J.
United States. National Advisory Committee for Aeronautics.

January 1948

This report presents a chart showing the results of a study to determine those factors of airplane d...

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. ...

Analysis of the flat-spin characteristics of a twin-jet swept-wing fighter airplane

Bowman, J. S., Jr.
Chambers, J. R.
Anglin, E. L.

September 1969

Factors affecting flat spin characteristics of fighter aircraft with horizontal tail surface

Exploratory study of the effects of wing-leading-edge modifications on the stall/spin behavior of a light general aviation airplane /

Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 05."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

Spin-tunnel investigation of the effects of mass and dimensional variations on the spinning characteristics of a low-wing single-vertical-tail model typical of personal-owner airplanes /

Klinar, Walter J.
Wilson, Jack H.
United States. National Advisory Committee for Aeronautics.

January 1951

This paper presents the results of a spin-tunnel investigation of a low-wing model typical of presen...

Investigation of the dynamic lateral stability and control characteristics of a model of a fighter airplane without a horizontal tail and equipped with either single or twin vertical tails /

Draper, John W.
Rose, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"November 15, 1949."Includes bibliographical references (p. 8).Mode of access: Internet

Static force tests of a model of a twin-jet fighter airplane for angles of attack from -10⁰ to 110⁰ and sideslip angles from -40⁰ to 40⁰ /

Anglin, Ernie L.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Static force tests of model of twin jet fighter aircraft at various angles of attack and sideslip an...

Flight investigation of the effect of tail configuration on stall, spin, and recovery characteristics of a low-wing general aviation research airplane /

Stough, H. Paul.
Sliwa, Steven M.
Patton, James M., Jr.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1987

Distributed to depository libraries in microfiche.NAS 1.60:2644.Techinal paper.Mode of access: Inter...

Klinar, Walter J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1956

A discussion is presented of the type of control manipulation and various techniques that may be req...

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

Effects of fuselage forebody geometry on low-speed lateral-directional characteristics of twin-tail fighter model at high angles of attack /

Carr, Peter C.
Gilbert, William P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.
Hugh L. Dryden Flight Research Center.

January 1979

"December 1979"--Cover."Langley Research Center.""Dryden Flight Research Center."Includes bibliograp...

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Summary of spin technology as related to light general-aviation airplanes /

Bowman, James S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

A summary was made of all NASA (and NACA) research and experience related to the spin and recovery c...

Flight measurements of aerodynamic loads on the horizontal tail surface of a fighter-type airplane /

Garvin, John B.
United States. National Advisory Committee for Aeronautics.

January 1947

A series of flight measurements of the loads applied to the horizontal tail surfaces of a fighter-ty...

Exhaust-nozzle characteristics for a twin-jet variable-wing-sweep fighter airplane model at Mach numbers to 2.2 /

Reubush, David E.
Mercer, Charles E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

The Influence of very heavy fuselage mass loadings and long nose lengths upon oscillations in the spin /

Stone, Ralph W.
Klinar, Walter J.
United States. National Advisory Committee for Aeronautics.

January 1948

This report presents a chart showing the results of a study to determine those factors of airplane d...

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. ...

Analysis of the flat-spin characteristics of a twin-jet swept-wing fighter airplane

Bowman, J. S., Jr.
Chambers, J. R.
Anglin, E. L.

September 1969

Factors affecting flat spin characteristics of fighter aircraft with horizontal tail surface

Exploratory study of the effects of wing-leading-edge modifications on the stall/spin behavior of a light general aviation airplane /

Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

Subject category 05."December 1979"--Cover.Includes bibliographical references.Mode of access: Inter...

Spin-tunnel investigation of the effects of mass and dimensional variations on the spinning characteristics of a low-wing single-vertical-tail model typical of personal-owner airplanes /

Klinar, Walter J.
Wilson, Jack H.
United States. National Advisory Committee for Aeronautics.

January 1951

This paper presents the results of a spin-tunnel investigation of a low-wing model typical of presen...

Investigation of the dynamic lateral stability and control characteristics of a model of a fighter airplane without a horizontal tail and equipped with either single or twin vertical tails /

Draper, John W.
Rose, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"November 15, 1949."Includes bibliographical references (p. 8).Mode of access: Internet

Static force tests of a model of a twin-jet fighter airplane for angles of attack from -10⁰ to 110⁰ and sideslip angles from -40⁰ to 40⁰ /

Anglin, Ernie L.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

Static force tests of model of twin jet fighter aircraft at various angles of attack and sideslip an...

Flight investigation of the effect of tail configuration on stall, spin, and recovery characteristics of a low-wing general aviation research airplane /

Stough, H. Paul.
Sliwa, Steven M.
Patton, James M., Jr.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1987

Distributed to depository libraries in microfiche.NAS 1.60:2644.Techinal paper.Mode of access: Inter...

Klinar, Walter J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1956

A discussion is presented of the type of control manipulation and various techniques that may be req...

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

Effects of fuselage forebody geometry on low-speed lateral-directional characteristics of twin-tail fighter model at high angles of attack /

Carr, Peter C.
Gilbert, William P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.
Hugh L. Dryden Flight Research Center.

January 1979

"December 1979"--Cover."Langley Research Center.""Dryden Flight Research Center."Includes bibliograp...

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Summary of spin technology as related to light general-aviation airplanes /

Bowman, James S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1971

A summary was made of all NASA (and NACA) research and experience related to the spin and recovery c...

Flight measurements of aerodynamic loads on the horizontal tail surface of a fighter-type airplane /

Garvin, John B.
United States. National Advisory Committee for Aeronautics.

January 1947

A series of flight measurements of the loads applied to the horizontal tail surfaces of a fighter-ty...

Exhaust-nozzle characteristics for a twin-jet variable-wing-sweep fighter airplane model at Mach numbers to 2.2 /

Reubush, David E.
Mercer, Charles E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

The Influence of very heavy fuselage mass loadings and long nose lengths upon oscillations in the spin /

Stone, Ralph W.
Klinar, Walter J.
United States. National Advisory Committee for Aeronautics.

January 1948

This report presents a chart showing the results of a study to determine those factors of airplane d...

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. ...

Analysis of the flat-spin characteristics of a twin-jet swept-wing fighter airplane /

Abstract

Extracted data

Analysis of the flat-spin characteristics of a twin-jet swept-wing fighter airplane /

Abstract

Extracted data

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