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Start Over Author "N. Sorensen" Publisher american institute of aeronautics and astronautics (aiaa)
3 results on '"N. Sorensen"'

3. Performance Estimates for a Supersonic Axisymmetric Inlet System

Author

N. Sorensen and D. Smeltzer

Subjects
geography, Engineering, Supersonic wind tunnel, geography.geographical_feature_category, business.industry, Rotational symmetry, Aerospace Engineering, Structural engineering, Mechanics, Bleed, Inlet, Diffuser (thermodynamics), symbols.namesake, Mach number, symbols, Performance prediction, Environmental science, Hypersonic wind tunnel, Supersonic speed, business, Wind tunnel
Abstract

Results of recent tests of a large-scale axisymmetric mixed-compression inlet system designed for Mach number 2.65 indicate that the performance of the supersonic diffuser and required boundary-layer bleed system can be accurately estimated with relatively new analytic methods. Thus, many wind tunnel testing hours can be saved by avoiding much of the usual ?cut and try' wind tunnel development.

Published
1972
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