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Accession Number:
AD0832027
Title:
AN EXPERIMENTAL INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF SLENDER HYPERSONIC VEHICLES AT HIGH ANGLES OF ATTACK
Corporate Author:
NAVAL ORDNANCE LAB WHITE OAK MD
Report Date:
1968-05-01
Abstract:
Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an inclined cone were obtained in a wind tunnel at a nominal Mach number of 6. Force measurements were also obtained for a 23 power law body and two ducted-cone configurations.
Descriptive Note:
Final rept.
Pages:
0119
Contract Number:
ARPA
Contract Number 2:
ORDER-905
File Size:
4.81MB
