A study of moderately underexpanded single and twinjet rocket exhaust plumes in quiescent and in a mach 7 hypersonic freestream

Rocket plume flowfields have an importance due to their influence on the signature of the rocket and also on the distribution of the plume gases around the vehicle. Little information on the co-flowing situation exists other than a previous study at Oxford. This thesis thus represents a significant...

Cur síos iomlán

Sonraí bibleagrafaíochta
Príomhchruthaitheoirí: Shek, H, Shek, Howard
Formáid: Tráchtas
Teanga:English
Foilsithe / Cruthaithe: 1997
Ábhair: