Predicting Temperature Rises, Due to Aerodynamic Heating: An Analogue Method Utilizing Trajectory Data to Calculate Temperature Distribution Throughout a Missile Radome

Author： B.A. D. Readshaw  

Publisher： Emerald Group Publishing Ltd

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.33, Iss.1, 1993-12, pp. : 8-11

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