Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket -propelled airplane configuration having a low 52.5 (degree) delta wing and an unswept horizontal tail [NASA TN D-836]
By: Kehlet, Alan B.
Material type:
BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D.C. Nasa 1961Description: 26p.Subject(s): Aerodynamic
Contents:
NASA technical report
| 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-836 (Browse shelf) | Not for loan | TR16137 |
Total holds: 0
NASA technical report
There are no comments for this item.