FLOW FIELD ANALYSIS OF AIRCRAFT CONFIGURATION USING A NUMERICAL SOLUTION TO THE THREE-DIMENSIONAL UNIFIED SUPERSONIC/HYPERSONIC SMALL-DISTURBENCE EQUATIONS
By: Gunness,C.
Material type:
BookPublisher: Nasa, Washington, D.C. 1972Description: 114.DDC classification: NASA | CR-1927
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | NASA CR-1927 (Browse shelf) | Not for loan | TR8347 |
Total holds: 0
Bound With Nasa Cr-1921-28
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