NASA Memorandum [NASA MEMO 4-21-59A]: Longitudinal stability and control characteristics at mach numbers from 0.70 to 2.22 of a triangular wing configuration equipped with a canard control, a trailing-edge-flap control or a cambered forebody
By: Washington. National Aeronautics and Space Administration (NASA).
Contributor(s): Boyd, John W | Menees, Gene P.
Material type:
BookSeries: National Aeronautics and Space Administration ; NASA Memorandum. Publisher: Washington NASA 1959Description: 39p.Subject(s): Longitudinal control devices --Tests
| 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 4-14-59A to 4-27-59A | Not for loan | TR11613 |
Total holds: 0
Bound together NASA MEMO 4-14-59A to 4-27-59A
Lack No.4-16 to 4-17, 4-22 to 4-25
Bound vol. Acc. No. 102439 contains Acc. No. TR11609 to TR11615
There are no comments for this item.