Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
4 results returnedSearch results
- Preliminary attempts at isothermal compression of a supersonic air stream
- An analog study of a shock-position diffuser control on a supersonic turbojet engine
- An inlet design concept to reduce flow distortion at angle of attack
- Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet