LOW-SPEED WIND-TUNNEL INVESTIGATION TO DETERMINE THE AERODYNAMIC CHARACTERISTICS OF A RECTANGULAR WING EQUIPPED WITH A FULL-SPAN AND AN INBOARD HALF-SPAN JET-AUGMENTED FLAP DEFLECTED 55 DEGREE
By: Gainer,Thomas G.
Material type:
BookPublisher: Nasa, Washington, D.C. 1959Description: 21.DDC classification: NASA | NEMO 1-27-59L
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | NASA NEMO 1-27-59L (Browse shelf) | Not for loan Untraceable | TR17741 |
Total holds: 0
Bound With Nasa Memo 1-15-59l-26,30-31, Lack No.1-18-59l-1-19-59l,1-21-59l,1-28-59l-1-29-59l
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