In-Tube Catapult Launch from Rectangular-Bore Aeroballistic Range

Author:

Sasoh Akihiro1,Imaizumi Takahiro1,Toyoda Atsushi1,Ooyama Takeshi1

Affiliation:

1. Department of Aerospace Engineering, Nagoya University, Nagoya 464-8603, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

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1. Numerical Investigation of a Ballistic Range Free Flight Model;International Journal of Aeronautical and Space Sciences;2021-08-23

2. Generation and Utilization of Compressible Flows;Compressible Fluid Dynamics and Shock Waves;2020

3. Near-Field Pressure Signature over Mach 1.7 Free-Flight Bodies;31st International Symposium on Shock Waves 2;2019

4. Behavior of Whole Near-Filed Flow over Mach 1.7 Free-Flight Bodies;35th AIAA Applied Aerodynamics Conference;2017-06-02

5. Near-Field Measurement of Post-Shock Pressure Modulation Induced by Supersonic Flight Model past a Grid Turbulence;34th AIAA Applied Aerodynamics Conference;2016-06-10

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