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Accession Number:
AD0670512
Title:
EXPANSION SIDE FLOW FIELD IMPACT PRESSURE SURVEYS OF A 75-DEG DELTA WING AT MACH NUMBER 10
Corporate Author:
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
Report Date:
1968-06-01
Abstract:
Impact pressure surveys were obtained in the leeward flow field of a 75-deg sharp leading-edge delta wing. Tests were conducted at a Mach number of 10.13, Reynolds number based on model length of 430,000, angles of attack of 15 and 19 deg, and zero sideslip angle. Abrupt pressure changes were observed in the flow field between the model surface and bow shock. Representative results are presented for alpha 15 deg.
Descriptive Note:
Final rept. 30 Nov-20 Dec 1967
Supplementary Note:
Prepared in cooperation with ARO, Inc., Tullahoma, TN.
Pages:
0016
Distribution Statement:
Approved for public release; distribution is unlimited.
Contract Number:
AF 40(600)-1200
File Size:
0.69MB
