Multiaxis thrust vectoring using axisymmetric nozzles and postexit vanes on an F/A-18 configuration vehicle [PDF]
A ground-based investigation was conducted on an operational system of multiaxis thrust vectoring using postexit vanes around an axisymmetric nozzle.
Bowers, Albion H. +4 more
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Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraft [PDF]
The internal performance of two exhaust system concepts applicable to single-engine short-take-off and vertical-landing tactical fighter configurations was investigated.
Carson, George T., Jr., Re, Richard J.
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A review of instability and noise propagation in supersonic flows [PDF]
Originally analytical and numerical models were to be developed for noise production in supersonic jets, wakes and free shear layers. While the effort was concentrated initially on these aspects, other topics were also pursued, most were of interest to ...
Daudpota, Q. Isa, Lakin, William D.
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An improved analytical model of the separation region on boattail nozzles at subsonic speeds [PDF]
A practical engineering calculation was developed to model the viscous effects of a separated, reverse flow region on afterbody pressures and drag.
Buteau, J. D. +2 more
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Effect of nozzle and vertical-tail variables on the performance of a 3-surface F-15 model at transonic Mach numbers [PDF]
An investigation was conducted in the Langley 16 foot transonic tunnel to determine the longitudinal aerodynamic characteristics of twin two dimensional nozzles and twin baseline axisymmetric nozzles installed on a fully metric 0.047 scale model of the F-
Bare, E. A., Pendergraft, O. C., Jr.
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A study of nozzle and ejector flow problems by the method of integral relations [PDF]
The application of the method of integral relations to nozzle and ejector flow problems was examined. For nozzle flow problems, the general formulation is that the approaching flow may be rotational.
Chow, W. L., Howlett, L. D.
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Simulation of transient flow in a shock tunnel and a high Mach number nozzle [PDF]
A finite volume Navier-Stokes code was used to simulate the shock reflection and nozzle starting processes in an axisymmetric shock tube and a high Mach number nozzle.
Jacobs, P. A.
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Mechanistic Investigation of Microdroplet Formation in High-Viscosity Shear-Thinning Hydrogel Bioinks. [PDF]
GelsGao Q +6 more
europepmc +1 more source
Instability of a supersonic shock free elliptic jet [PDF]
This paper presents a comparison of the measured and the computed spatial stability properties of an aspect ratio 2 supersonic shock free elliptic jet.
Baty, Roy S. +2 more
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Direct Numerical Simulation of Acoustic Disturbances in the Rectangular Test Section of a Hypersonic Wind Tunnel [PDF]
Direct numerical simulations (DNS) of the full-scale rectangular nozzle of a hypersonic wind tunnel are conducted to study the acoustic freestream fluctuations radiating from turbulent boundary layers (TBLs) along the nozzle walls.
Choudhari, Meelan M. +3 more
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