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

Stability and control characteristics of an air-breathing missile configuration having a forward located inlet /

Sawyer, Wallace C.
Hayes, Clyde.
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Wind-tunnel investigation to determine the low-speed yawing stability derivatives of a twin-jet fighter model at high angles of attack /

Coe, Paul L.
Newsom, William A.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

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

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

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. ...

Effect of several tail configurations on the stability characteristics of a midwing supersonic-bomber model at mach numbers of 1.60, 1.90, 2.20, and 2.50 /

Wells, R. Franklin.
Silvers, H. Norman.
Langley Research Center.

January 1960

"Langley Research Center, Langley Field, Va.""NASA TM X-279."Cover title.Mode of access: Internet

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

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...

Aerodynamic roll damping of a T-tail transport configuration /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /

Lamb, Milton.
Thomas, James L. (James Lee), 1952-
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Investigation at high subsonic speeds of the use of low auxiliary tail surfaces having dihedral to improve the longitudinal and directional stability of a T-tail model at high lift. /

Sleeman, William C.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Subsonic maneuver capability of a supersonic cruise fighter wing concept /

Riebe, Gregory D.
Fox, Charles H.
Langley Research Center.

January 1987

Prepared at Langley Research Center."January 1987"--Cover.Includes bibliographical references (p. 10...

Investigation of the subsonic stability and control characteristics of a 1/7-scale model of the North American X-15 airplane with and without fuselage forebody strakes /

Hassell, James L.
Hewes, Donald E.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Low-subsonic-speed static longitudinal stability and control characteristics of a winged reentry-vehicle configuration having wingtip panels that fold up for high-drag reentry /

Ware, George M.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 5).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

Stability and control characteristics of an air-breathing missile configuration having a forward located inlet /

Sawyer, Wallace C.
Hayes, Clyde.
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Wind-tunnel investigation to determine the low-speed yawing stability derivatives of a twin-jet fighter model at high angles of attack /

Coe, Paul L.
Newsom, William A.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

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

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

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. ...

Effect of several tail configurations on the stability characteristics of a midwing supersonic-bomber model at mach numbers of 1.60, 1.90, 2.20, and 2.50 /

Wells, R. Franklin.
Silvers, H. Norman.
Langley Research Center.

January 1960

"Langley Research Center, Langley Field, Va.""NASA TM X-279."Cover title.Mode of access: Internet

Supersonic aerodynamic characteristics of canard, tailless, and aft-tail configurations for two wing planforms /

Covell, Peter F.
Langley Research Center.

January 1985

Prepared at Langley Research Center."June 1985"--Cover.Includes bibliographical references (p. 66).M...

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...

Aerodynamic roll damping of a T-tail transport configuration /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 12).Mode of ...

Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /

Lamb, Milton.
Thomas, James L. (James Lee), 1952-
Sawyer, Wallace C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Investigation at high subsonic speeds of the use of low auxiliary tail surfaces having dihedral to improve the longitudinal and directional stability of a T-tail model at high lift. /

Sleeman, William C.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

Subsonic maneuver capability of a supersonic cruise fighter wing concept /

Riebe, Gregory D.
Fox, Charles H.
Langley Research Center.

January 1987

Prepared at Langley Research Center."January 1987"--Cover.Includes bibliographical references (p. 10...

Investigation of the subsonic stability and control characteristics of a 1/7-scale model of the North American X-15 airplane with and without fuselage forebody strakes /

Hassell, James L.
Hewes, Donald E.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Low-subsonic-speed static longitudinal stability and control characteristics of a winged reentry-vehicle configuration having wingtip panels that fold up for high-drag reentry /

Ware, George M.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 5).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

Stability and control characteristics of an air-breathing missile configuration having a forward located inlet /

Sawyer, Wallace C.
Hayes, Clyde.
Langley Research Center.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 9).Mode of a...

Wind-tunnel investigation to determine the low-speed yawing stability derivatives of a twin-jet fighter model at high angles of attack /

Coe, Paul L.
Newsom, William A.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 8).Mode of a...

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds /

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

January 1979

"October 1979"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: ...

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

Abstract

Extracted data

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

Abstract

Extracted data

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