Drag and heat reduction mechanism induced by a combinational novel cavity and counterflowing jet concept in hypersonic flows
Author:
Funder
Science Foundation of National University of Defense Technology
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference42 articles.
1. A survey of drag and heat reduction in supersonic flows by a counterflowing jet and its combinations;Huang;J Zhejiang Univ. – Sci. A (Appl. Phys. Eng.),2015
2. Nummerical simulation in influence of forward-facing cavity on aerodynamic heating of hypersonic vehicle;Lu;Procedia Eng.,2012
3. Measurements of resonance in a forward-facing cavity at Mach six;Chou;J. Spacecr. Rocket.,2015
4. Investigation of missile-shaped body with forward-facing cavity at Mach 8;Saravanan;J. Spacecr. Rocket.,2009
5. Drag reduction research in supersonic flow with opposing jet;Rong;Acta Astronaut.,2013
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