Cover Image

Crossflow in two-dimensional asymmetric nozzles/

Main Author:	Sebacher, Daniel I.
Corporate Authors:	United States National Aeronautics and Space Administration, United States. National Aeronautics and Space Administration, Langley Research Center
Other Authors:	Lee, Louise P.
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, 1975
Series:	NASA technical note 7999
Subjects:	Jet nozzles Jets > Fluid dynamics

Similar Items

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)

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

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

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

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)

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)

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

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

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

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)

Static investigation of a two-dimensional convergent-divergent exhaust nozzle with multiaxis thrust-vectoring capability/
by: Taylor, John G.
Published: (1990)

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

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)

Capillary and acceleration wave breakup of liquid jets in axial-flow airstreams/
by: Ingebo, Robert D.
Published: (1981)

The effects on propulsion-induced aerodynamic forces of vectoring a partial-span rectangular jet at mach numbers from 0.40 to 1.20/
by: Capone, Francis J.
Published: (1975)

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

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

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

Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers
by: Pendergraft, Odis C.
Published: (1982)

Boundary-layer separation on isolated boattail nozzles/
by: Abeyounis, William Kelly
Published: (1978)

Proceedings of the 2001 WJTA American Waterjet Conference : August 18-21, 2001, Minneapolis, Minnesota /
Published: (2001)

An overview of waterjet fundamentals and applications /
Published: (2001)

Venturi nozzle effects on fuel drop size and nitrogen oxide emissions/
by: Johnson, Susan M. 1952-
Published: (1982)

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

Jet array impingement flow distributions and heat transfer characteristics : effects of initial crossflow and nonuniform array geometry /
Published: (1982)

Turbulent jets/
by: Rajaratnam, N.
Published: (1976)

Liquid jet impingement normal to a disk in Zero gravity/
by: Labus, Thomas L.
Published: (1977)

Proceedings of the 10th American Waterjet Conference : August 14-17, 1999, Houston, Texas /
Published: (2001)

Fluid dynamics of jets with applications to V/STOL
Published: (1982)

Acoustically excited heated jets/
Published: (1988)

Fluid dynamics of jet amplifiers : course held at the Department of Hydro- and Gasdynamics, September 1970 /
by: Romiti, Ario
Published: (1970)

Effect of a simulated engine jet blowing above an arrow wing at mach 2.0/
by: Shrout, Barrett L.
Published: (1978)

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

Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles/
by: Head, Verlon L.
Published: (1984)

Static and wind-on tests of an upper-surface-blown jet-flap nozzle arrangement for use on the Quiet Clean Shore-haul Experimental Engine (QCSEE)/
by: Phelps, Arthur E.
Published: (1977)

Fully-coupled analysis of jet mixing problems : three-dimensional PNS model, SCIP3D /
by: Wolf, D. E.
Published: (1988)

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

Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20/
by: Carson, George T.
Published: (1988)

A finite-difference analysis of the nozzle starting process in an expansion tunnel/
by: Weilmuenster, K. James
Published: (1975)

Static internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzles/
by: Leavitt, Laurence D.
Published: (1982)

Cannot write session to /tmp/vufind_sessions/sess_cfdlmfm8nkb5uohhggk3jsd1m0