NASA Technical Note [NASA TN D-4909]: Effects of angle of attack and bluntness on the shock-layer properties of a 15 degree cone at a mach number of 10.6
By: Washington. National Aeronautics and Space Administration (NASA).
Contributor(s): Cleary, Joseph W.
Material type:
BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington NASA 1968Description: 38p.Subject(s): Aeronautics | Aircraft -- Conical bodies -- Flow distribution | Aircraft -- Shock layers -- Angle of attack and bluntness
| 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 TN D-4900 to 4910 | Not for loan | TR13267 |
Total holds: 0
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Bound together NASA TN D-4900 to 4910
Bound vol. Acc. No. 101121 contains Acc. No. TR13259 to TR13268
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