Cover Image

Static investigation of a two-dimensional convergent-divergent exhaust nozzle with multiaxis thrust-vectoring capability/

Main Author:	Taylor, John G.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Division, United States. National Aeronautics and Space Administration. Scientific and Technical Information Division, Langley Research Center
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990
Series:	NASA technical paper 2973
Subjects:	Jet nozzles Aircraft exhaust emissions

Similar Items

Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring/
by: Bare, E. Ann
Published: (1987)

Simulation of a hydrocarbon fueled scramjet exhaust/
by: Leng, J.
Published: (1982)

Static internal performance including thrust vectoring and reversing of tow-dimensional convergent-divergent nozzles/
by: Re, Richard J.
Published: (1984)

Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles/
by: Yetter, Jeffery A.
Published: (1980)

Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap/
by: Re, Richard J.
Published: (1986)

Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability/
by: Mason, Mary L.
Published: (1986)

Effects of jet exhaust gas properties on exhaust simulation and afterbody drag/
by: Compton, William B.
Published: (1975)

Crossflow in two-dimensional asymmetric nozzles/
by: Sebacher, Daniel I.
Published: (1975)

Internal performance of two nozzles utilizing gimbal concepts for thrust vectoring/
by: Berrier, Bobby L.
Published: (1990)

Experimental and analytical investigation of a nonaxisymmetric and wedge nozzle at static conditions/
by: Carson, George T.
Published: (1978)

Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20/
by: Capone, Francis J.
Published: (1977)

Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20/
by: Carson, George T.
Published: (1984)

Parametric experimental investigation of a scramjet nozzle at Mach 6 with freon and argon or air used for exhaust simulation/
by: Cubbage, James M.
Published: (1991)

Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes/
by: Mason, Mary L.
Published: (1988)

Aircraft engine emissions : a conference held at Lewis Research Center, Cleveland, Ohio, May 18-19, 1977
Published: (1977)

In situ measurements of Arctic atmospheric trace constituents from an aircraft/
by: Reck, Gregory M.
Published: (1977)

Estimating takeoff thrust settings for airport emissions inventories
Published: (2015)

Validation of scramjet exhaust simulation technique at Mach 6/
by: Hopkins, H. B.
Published: (1979)

Environmental effects from SRB exhaust effluents : technique development and preliminary assessment /
Published: (1977)

Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps/
by: Leavitt, Laurence D.
Published: (1982)

Site alteration effects from rocket exhaust impingement during a simulated Viking Mars landing/
Published: (1973)

Effect of primary zone equivalence ratio on pollutant formation/
by: Claus, Russell W.
Published: (1979)

Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle/
by: Carson, George T.
Published: (1987)

Aeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model/
by: Capone, Francis J.
Published: (1982)

Simulation of hypersonic scramjet exhaust/
Published: (1975)

Experimental investigation of close-range rocket-exhaust impingement on surfaces/
by: Clark, Leonard V.
Published: (1970)

Statis performance of five twin-engine nonaxisymmetric nozzles with vectoring and reversing capability/
by: Capone, Francis J.
Published: (1978)

Static and wind tunnel near-field/far-field jet noise measurements from model scale single-flow baseline and suppressor nozzles
by: Jaeck, Carl L.
Published: (1977)

Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20/
by: Capone, Francis J.
Published: (1991)

Some physical and thermodynamic properties of rocket exhaust clouds measured with infrared scanners/
by: Gomberg, Richard I.
Published: (1977)

Interim review of the subsonic assessment project : management, science, and goals /
Published: (1997)

Atmospheric effects of aviation a review of NASA's subsonic assessment project /
Published: (1999)

Best practices guidebook for preparing lead emission inventories from piston-powered aircraft with the Emission Inventory Analysis Tool /
by: Heiken, Jeremy.
Published: (2015)

Performance of an isolated two-dimensional variable-geometry wedge nozzle with translating shroud and collapsing wedge at speeds up to mach 2.01/
by: Maiden, Donald L.
Published: (1975)

Exhaust emission calibration of two J-58 afterburning turbojet engines at simulated high-altitude, supersonic flight conditions/
by: Holdeman, James D.
Published: (1976)

Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts/
by: Berrier, Bobby L.
Published: (1979)

Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles/
by: Mason, Mary L.
Published: (1985)

Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft/
by: Berrier, Bobby L.
Published: (1980)

Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model/
by: Reubush, David E.
Published: (1975)

Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles : theory /
by: Thomas, P. D. 1935-
Published: (1979)

Cannot write session to /tmp/vufind_sessions/sess_33p4is4f34pa1p9gt8ss11o5e4