Experimental Investigation Of Shock Wave Turbulent Boundary Layer Interactions In Axisymmetric Flow At Mach 380 Including Suction Effects
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Aeronautical Engineering
| Author | : |
| Publisher | : |
| Total Pages | : 1020 |
| Release | : 1992 |
| Genre | : Aeronautics |
| ISBN | : |
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
