Effects of body-mounted lateral controls and speed brakers the aerodynamic load distribution over a 45 degree swept wing at mach numbers from 0.80 to 0.90. [NASA TN D-522]
By: West, F. E.
Material type:
BookPublisher: NASA Washington, D.C. 1960Description: various pagings.
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | NASA TN D-522 (Browse shelf) | Not for loan | TR15667 |
Total holds: 0
Bound With NASA TN D-521,523-530.
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