LOW-SUBSONIC STATIC STABILITY AND DAMPING DERIVATIVES AT ANGLES OF ATTACK FROM 0 DEGREE TO 90 DEGREE FOR A MODEL WITH A LOW-ASPECT-RATIO UNSWEPT WING AND TWO DIFFERENT FUSELAGE FOREBODIES
By: Boisseau,Peter C.
Material type:
BookPublisher: Nasa, Washington, D.C. 1959Description: 25.DDC classification: NASA | MEMO 1-22-59L
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | NASA MEMO 1-22-59L (Browse shelf) | Not for loan | TR17736 |
Total holds: 0
Bound With Nasa Memo 1-15-59l-20,23-31 Lack No.1-18-59l-1-19-59l,1-21-59l,1-28-59l-1-29-59l
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