DYNAMIC STABILITY DERIVATIVES OF A SLENDER WING, A COMPARISON OF THEORY WITH FREE-FLIGHT MODEL TESTS AT NEAR-ZERO LIFT M = 0.8 TO 2.4
By: Turner,K. J., Ross,A. Jean.
Contributor(s): Earley,Geraldine.
Material type:
BookPublisher: Her Majesty'S Stationery Office, London 1968Description: 67.DDC classification: HMSO-R&M-995 | -
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | HMSO-R&M-995 - (Browse shelf) | Not for loan Untraceable | TR9652 |
Total holds: 0
Bound With Hmso-R&M-991-99
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