Neasurement of aerodynamics heat transfer to a deflected trailing edge flap on a delta fin in free flight at Mach numbers from 1.5 to 2.6 [NASA Tn D-250]
By: Chauvin, Leo T. and Buglia James J.
Contributor(s): Buglia James J.
Material type:![materialTypeLabel](/opac-tmpl/lib/famfamfam/BK.png)
Contents:
Technical note D-250
Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
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PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | Not for loan | 63648 D-250 |
Total holds: 0
Technical note D-250
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