The vortical flow on the leeward side of a delta-wing model has been visualized at several different tunnel conditions in the NASA Langley 0.3-Meter Transonic Cryogenic Tunnel using a vapor-screen flow-visualization technique. Vapor-screen photographs of the subject flow field are presented and interpreted relative to phenomenological implications. Results indicate that the use of nitrogen fog in conjunction with the vapor-screen technique is feasibile.
Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel
1986-05-01
Report
Keine Angabe
Englisch
Application of FLEET Velocimetry in the NASA Langley 0.3-meter Transonic Cryogenic Tunnel
British Library Conference Proceedings | 2015
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