Effects of counterflow jet on the performance of a generic rocket at Mach 4 to 9

Author:

Ölçmen Semih,Reasor Daniel

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. Numerical and experimental analysis of projectile nose geometry;Schinetsky;AIAA J. Spacecraft Rockets,2015

2. Minimum drag and heating 0.3-caliber projectile nose geometry;Ölçmen;Proc IMechE Part C: J. Mech. Eng. Sci.,2019

3. Effects of counterflow jet on the performance of a generic rocket;Ölçmen;Acta Astronaut.,2021

4. Evolutionary algorithm shape optimization of a hypersonic flight experiment nose cone;Deepak;J. Spacecraft Rockets,2008

5. Hypersonic lifting body aerodynamic shape optimization based on the multiobjective evolutionary algorithm based on decomposition;Ma;J. Aero. Eng.,2015

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