Hypersonic boundary layer instability measurements at Mach 7 and flight total enthalpy

This paper presents boundary layer instability measurements obtained in The University of Queensland’s T4 Stalker Tunnel at Mach 7. The model geometry is a 7◦ half angle cone with a nose bluntness of 1.55 mm radius, pitched at an angle of attack of zero degrees. Results are presented at a constant e...

সম্পূর্ণ বিবরণ

গ্রন্থ-পঞ্জীর বিবরন
প্রধান লেখক: Wylie, S, McGilvray, M, Raghunath, S, Mee, D
বিন্যাস: Conference item
ভাষা:English
প্রকাশিত: 2019