NASA Memo [10-2-58L] : AERODYNAMIC CHARACTERISTICS FOR COMBINED ANGLES OF ATTACK AND SIDESLIP OF A LOW-ASPECT-RATIO CRUCIFORM-WING MISSILE CONFIGURATION EMPLOYING VARIOUS CANARD AND TRAILING-EDGE FLAP CONTROLS AT A NO.2.01
By: Robinson, Ross B.
Contributor(s): Spearman, M. Leroy.
Series: NASA Memorandum. Publisher: Washington National Aeronautics and Space Administration 1958Description: 71p.Subject(s): Aerodynamics| Item type | Current location | Collection | Call number | Vol info | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | NASA MEMO-10-2-58L | Not for loan | TR8572 |
Total holds: 0
NASA Memorandum 10-1-58L-10-17-58L
Bound Vol. No.102461; Contents: TR-8572-8580
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