Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards /

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes /

Mason, Mary L.
Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 10).Mo...

Flap effectiveness on subsonic longitudinal aerodynamic characteristics of a modified arrow wing /

Quinto, P. Frank.
Paulson, John W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

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

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring /

Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 11).Mo...

Aeropropulsive characteristics of twin nonaxisymmetric vectoring nozzles installed with forward swept and aft-swept wings /

Capone, Francis J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."March 1981"--Cover.Includes bibliographical references.Mode of access: Internet

Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 /

Carson, George T.
Lamb, Milton.
Langley Research Center.

January 1988

Prepared at Langley Research Center."June 1988"--Cover.Includes bibliographical references (p. 13).M...

Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20 /

Capone, Francis J.
Mason, Mary L.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Chiefly statistical tables.Bibliography: p. 13.Mode of access: I...

Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing /

Re, Richard J.
Berrier, Bobby L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 02."March 1982"--Cover."Langley Research Center."Includes bibliographical reference...

Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft /

Capone, Francis J.
Reubush, David E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

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

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

Investigation of installation effects on twin-engine convergent-divergent nozzles /

Bare, E. Ann.
Berrier, Bobby L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."November 1983"--Cover.Distributed to depository libraries in microfiche.Include...

Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20 /

Carson, George T.
Mason, Mary L.
Capone, Francis J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 02.Distributed to depository libraries in microfiche."May 1984"--Cover.Includes bib...

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 ...

Experimental study of aeroelastic instability of overexpanded rocket nozzle extensions /

Tuovila, W. J. (Weimer J.)
Land, Norman S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 6).Mode of access: Internet

Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics /

Leavitt, Laurence D.
Bare, E. Ann.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"May 1983"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical referen...

Aerodynamic characteristics of four-duct tandem VTOL-aircraft configurations /

Newsom, William A.
United States. National Aeronautics and Space Administration.

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

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes /

Mason, Mary L.
Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 10).Mo...

Flap effectiveness on subsonic longitudinal aerodynamic characteristics of a modified arrow wing /

Quinto, P. Frank.
Paulson, John W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

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

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring /

Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 11).Mo...

Aeropropulsive characteristics of twin nonaxisymmetric vectoring nozzles installed with forward swept and aft-swept wings /

Capone, Francis J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 02."March 1981"--Cover.Includes bibliographical references.Mode of access: Internet

Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 /

Carson, George T.
Lamb, Milton.
Langley Research Center.

January 1988

Prepared at Langley Research Center."June 1988"--Cover.Includes bibliographical references (p. 13).M...

Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20 /

Capone, Francis J.
Mason, Mary L.
Langley Research Center.

January 1991

Prepared at Langley Research Center.Chiefly statistical tables.Bibliography: p. 13.Mode of access: I...

Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing /

Re, Richard J.
Berrier, Bobby L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 02."March 1982"--Cover."Langley Research Center."Includes bibliographical reference...

Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft /

Capone, Francis J.
Reubush, David E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

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

Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers /

Dunham, Dana Morris.
Langley Research Center.

January 1987

Prepared at Langley Research Center."October 1987"--Cover.Includes bibliographical references (p. 57...

Investigation of installation effects on twin-engine convergent-divergent nozzles /

Bare, E. Ann.
Berrier, Bobby L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 02."November 1983"--Cover.Distributed to depository libraries in microfiche.Include...

Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20 /

Carson, George T.
Mason, Mary L.
Capone, Francis J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 02.Distributed to depository libraries in microfiche."May 1984"--Cover.Includes bib...

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 ...

Experimental study of aeroelastic instability of overexpanded rocket nozzle extensions /

Tuovila, W. J. (Weimer J.)
Land, Norman S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 6).Mode of access: Internet

Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics /

Leavitt, Laurence D.
Bare, E. Ann.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"May 1983"--Cover.Distributed to depository libraries in microfiche.Includes bibliographical referen...

Aerodynamic characteristics of four-duct tandem VTOL-aircraft configurations /

Newsom, William A.
United States. National Aeronautics and Space Administration.

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

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes /

Mason, Mary L.
Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 10).Mo...

Flap effectiveness on subsonic longitudinal aerodynamic characteristics of a modified arrow wing /

Quinto, P. Frank.
Paulson, John W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

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

Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring /

Berrier, Bobby L.
Langley Research Center.

January 1988

Prepared at Langley Research Center."May 1988"--Cover.Includes bibliographical references (p. 11).Mo...

Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards /

Abstract

Extracted data

Aeropropulsive characteristics of twin single-expansion-ramp vectoring nozzles installed with forward-swept wings and canards /

Abstract

Extracted data

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