DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click
HERE to register or log in.
Accession Number:
AD0288457
Title:
SUPERSONIC FLOW PAST AXIALLY SYMMETRIC BLUNT BODIES WITH A DETACHED SHOCK WAVE
Corporate Author:
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Report Date:
1962-05-11
Pages:
0001
File Size:
0.00MB