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1
Inlet and airframe compatibility for a V/STOL fighter/attack aircraft with top-mounted inlets by Durston, D. A.
Published 1982Call Number: Loading…
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2
Wave drag and high-speed performance of supersonic STOVL fighter configurations by Durston, D. A.
Published 1988Call Number: Loading…
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3
LinAir:a multi-element discrete vortex Weissinger aerodynamic prediction method by Durston, D. A.
Published 1993Call Number: Loading…
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4
Experimental and computational sonic boom assessment of Boeing N+2 low boom models / by Durston, D. A.
Published 2015Call Number: Loading…Online Access
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Government Document eBook -
5
Nozzle plume/shock interaction experimental and computational sonic boom analyses from the NASA Ames 9-by 7-foot supersonic wind tunnel / by Durston, D. A.
Published 2018Call Number: Loading…Online Access
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Government Document eBook
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