General Three-Dimensional Relation for Oblique Shocks on Swept Ramps-Reference-Cited by-同舟云学术

General Three-Dimensional Relation for Oblique Shocks on Swept Ramps

Published:2016-01 Issue:1 Volume:54 Page:310-319
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Domel Neal D.¹

Affiliation:

1. Propulsion Systems and CFD Technologies, Lockheed Martin Aeronautics Company, Fort Worth, Texas 76101

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J054230

Reference4 articles.

1. “Equations, Tables, and Charts for Compressible Flow,” NASA Ames Research Lab. Rept. 1135, Moffett Field, CA, 1953.

2. AndersonJ. D.Jr., Modern Compressible Flow with Historical Perspective, McGraw–Hill, New York, 1982, pp. 88–95.

3. ZucrowM. J.HoffmanJ. D., Gas Dynamics, Vol. 1, Wiley, New York, 1976, pp. 356–361.

4. HartleyT. T.BrandisR.MossayebiF. “Exact and Approximate Solutions to the Oblique Shock Equations for Real-Time Applications,” NASA CR-187173, 1991.

Cited by 7 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. Effect of unsteady supersonic flow on detonation under different hot jet initiation conditions;International Journal of Hydrogen Energy;2024-01

2. Numerical study of detonation propagation under the action of supersonic pulsating flow in expanding combustor;Acta Astronautica;2023-10

3. Detonation stabilization in supersonic expanding channel with velocity gradients;Physics of Fluids;2023-07-01

4. Effects of velocity shear layer on detonation propagation in a supersonic expanding combustor;Physics of Fluids;2021-10

5. An inviscid analysis of swept oblique shock reflections;Journal of Fluid Mechanics;2020-03-17