Hypersonic flow over a cone with nose cavity-Reference-Cited by-同舟云学术

Hypersonic flow over a cone with nose cavity

Published:1987-06-08 Issue: Volume: Page:
ISSN:
Container-title:19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference
language:
Short-container-title:

Author:

SAMBAMURTHI J.¹,HUEBNER L.¹,UTREJA L.¹

Affiliation:

1. BDM Corp., Huntsville,AL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1987-1193

Reference15 articles.

1. Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder a t a Mach Number Range of 2.49 to 4.44 ",NASA TMX-221. 1959.

2. Carter, Howard S. and Bressette, Ilalter D. " Heat-Transfer and Pressure Distribution on Six Blunt Noses a t a Mach Number of 2 ",NACA RM L57C18, April 1957.

3. bhachevsky, Ihor D. and Kostoff, Ronald N. 'I Supersonic Flow over Convex and Concave Shapes with Radiation and Ablation Effects", AIAA Journal, Yo 1 10. No 8. August 1972.

4. Unsteady solution of the flowfield over concave bodies

Cited by 15 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Review of wave drag reduction techniques: Advances in active, passive, and hybrid flow control;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-03-12

2. Heat flux characteristics within and outside a forward facing cavity in a hypersonic flow;Experimental Thermal and Fluid Science;2018-10

3. Forecasting Method of Shock-Standoff Distance for Forward-Facing Cavity;Shock Wave Interactions;2018

4. Experimental investigation on drag and heat flux reduction in supersonic/hypersonic flows: A survey;Acta Astronautica;2016-12

5. Aerodynamic Heating of a Hypersonic Projectile with Forward-Facing Ellipsoid Cavity at Nose;Journal of Spacecraft and Rockets;2015-01