Comparison of prediction methods and studies of relaxation in hypersonic turbulent nozzle-wall boundary layers [PDF]
Turbulent boundary layer measurements on axisymmetric hypersonic nozzle ...
Bushnell, D. M. +3 more
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Design of optimized three-dimensional thrust nozzle contours [PDF]
Design of optimized three-dimensional thrust nozzle ...
Murthy, S. N. B., Thompson, H. D.
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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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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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Solid rocket booster internal flow analysis by highly accurate adaptive computational methods [PDF]
The primary objective of this project was to develop an adaptive finite element flow solver for simulating internal flows in the solid rocket booster. Described here is a unique flow simulator code for analyzing highly complex flow phenomena in the solid
Bass, J. M. +5 more
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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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Airframe/propulsion integration characteristics at transonic speeds [PDF]
The aerodynamic characteristics for both single and twin-engine high-performance aircraft are significantly affected by shock induced flow interactions as well as other local flow interference effects which usually occur at transonic speeds.
Berrier, Bobby L., Henderson, William P.
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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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Specific Dynamic Parameters: A Novel Multi-View Stereo Vision Measurement System for Vector Nozzle. [PDF]
Sensors (Basel)Lin Z +6 more
europepmc +1 more source
Computation of supersonic jet mixing noise for an axisymmetric CD nozzle using k-epsilon turbulence model [PDF]
The turbulent mixing noise of a supersonic jet is calculated for a round convergent-divergent nozzle at the design pressure ratio. Aerodynamic computations are performed using the PARC code with a k-epsilon turbulence model.
Khavaran, Abbas +2 more
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