Launch Dynamics of Supersonic Projectiles-Reference-Cited by-同舟云学术

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Launch Dynamics of Supersonic Projectiles

Published:2013-11 Issue:6 Volume:50 Page:1150-1161
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Muthukumaran C. K.¹,Rajesh G.²,Kim H. D.³

Affiliation:

1. Department of Aerospace, Indian Institute of Space Science and Technology, Trivandrum, Kerala 695 547, India

2. Department of Mechanical and Automotive Engineering, Keimyung University, Daegu 704-701, Republic of Korea

3. School of Mechanical Engineering, Andong National University, Gyeongsangbuk-do 760-749, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A32466

Reference24 articles.

1. Numerical study on blast flowfields induced by supersonic projectiles discharged from shock tubes

2. Wave dynamic processes induced by a supersonic projectile discharging from a shock tube

3. WatanabeR.FujiiK.HigashinoF. “Numerical Solutions of the Flow Around a Projectile Passing Through a Shock Wave,” AIAA Paper 95-1790, 1995.

4. Projectile Aerodynamics Overtaking a Shock Wave

5. A study of unsteady projectile aerodynamics using a moving coordinate method

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