Comparison of aerodynamic coefficients obtained from theoretical calculations wind tunnel tests and flight tests data reduction for the alpha jet aircraft : The methods by which aerodynamic coefficients are determined and discussed. These include: calculations, wind tunnel experiments and experiments in flight for various prototypes of the Alpha Jet. A comparison of obtained results shows good correlation between expectations and in-flight test results.
By: Guiot, R.
Contributor(s): Wunnenberg, H.
Material type:
BookSubject(s): NASA Technical ReportDDC classification: NASA | TM-75237
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | NASA TM-75237 (Browse shelf) | Not for loan | A71053 |
Total holds: 0
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