EFFECT OF WING-TAILPLANE AERODYNAMIC INTERACTION ON TAIL FLUTTER
By: Williams,D. E.
Material type:
BookPublisher: Her Majesty'S Stationery Office, London 1958Description: 24.DDC classification: HMSO-R&M-3065 | -
| 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-3065 - (Browse shelf) | Not for loan | TR8908 |
Total holds: 0
Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: General Stacks Close shelf browser
| HMSO-R&M-3062 - EXPERIMENTAL INVESTIGATION OF THE EFFECT OF ENGINE LOADS ON WING STRUCTURES | HMSO-R&M-3063 - SAMPLING ERRORS OF ATMOSPHERICTURBULENCE MEASUREMENTS | HMSO-R&M-3064 - EXPERIMENTS ON TWO-DIMENSIONAL BASE FLOW AT M = 2.4 | HMSO-R&M-3065 - EFFECT OF WING-TAILPLANE AERODYNAMIC INTERACTION ON TAIL FLUTTER | HMSO-R&M-3067 - SUPERSONIC FLOW PAST QUASI-CYLINDRICAL BODIES OF ALMOST CIRCULAR CROSS-SECTION | HMSO-R&M-3068 - CALCULATED DERIVATIVES FOR RECTANGULAR WINGS OSCILLATING IN COMPRESSIBLE SUBSONIC FLOW | HMSO-R&M-3069 - OPTICS OF THE MACH-ZEHNDER INTERFEROMETER |
Bound With Hmso-R&M-3050-69
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