Evaluation by step response tests of prototype relief valves designed for YF-12 inlet stability bleed system
Language: English Series: NASA TM X 3262 : 1975Publication details: Washington, D.C. ; National Aeronartics and Space Administration ; 1975Edition: Description: 45 p; ISBN: Subject(s): | Supersonic inlets, Shock stability, Jet engine inlets, Air intaakesOnline resources: Click here to access onlineItem type | Current library | Call number | Status | Date due | Barcode | Item holds |
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Central Library, IITB | LNASA TM X 3262 : 1975 | Not for loan | A32652 |
Total holds: 0
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