A numerical analysis of the use of perforated walls to control shock location and moment in an internal compression supersonic inlet [NASA TR R-317]
By: Matthews, Clarence W.
Material type: BookSeries: National Aeronautics and Space Administration. Publisher: Washington, D. C. National Aeronautics and Space Administration 1969Description: 52p.Subject(s): Supersonic inletItem type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
---|---|---|---|---|---|---|---|
Reference | PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | Not for loan | tr002220 [R-317] |
Total holds: 0
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