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:
AD0215409
Title:
TWO-DIMENSIONAL CIRCULATION CONTROL TESTS ON A NACA 23015 AIRFOIL EQUIPPED WITH A SEALED AND SLOTTED FLAP TO DETERMINE JET MOMENTUM LOSS OVER THE FLAP
Corporate Author:
WICHITA STATE UNIV KS SCHOOL OF ENGINEERING
Report Date:
1958-12-01
Descriptive Note:
Engineering rept.,
Supplementary Note:
Supplement to Rept. no. 311, AD-215 408. Prepared in cooperation with Fairchild Engine and Airplane Corp. Hagerstown, Md. Rept. no. R246A-003-Suppl.
Pages:
0073
Contract Number:
Nonr-2226(00)
File Size:
0.00MB
