Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?

Because of their ubiquitous presence in high-speed flight and their impact on vehicle and component performance, shock-wave/boundary-layer interactions have been studied for about 50 years. Despite remarkable progress in computational measurement capabilities, there are still important quantities th...

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Veröffentlicht in:	AIAA journal 2001-08, Vol.39 (8), p.1517-1531
1. Verfasser:	Dolling, David S
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Compressible flows shock and detonation phenomena Computational fluid dynamics Computer simulation Exact sciences and technology Flight simulation Fluid dynamics Fundamental areas of phenomenology (including applications) Mathematics Nozzles Physics Predictions Pressure effects Shock waves Shock-wave interactions and shock effects Shock-wave interactions and shockeffects Thermal load
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Beschreibung
Zusammenfassung:	Because of their ubiquitous presence in high-speed flight and their impact on vehicle and component performance, shock-wave/boundary-layer interactions have been studied for about 50 years. Despite remarkable progress in computational measurement capabilities, there are still important quantities that cannot be predicted very accurately. Some suggestions are made as to where future research efforts might be focused.
ISSN:	0001-1452 1533-385X
DOI:	10.2514/2.1476