A method for calculating aerodynamic heating on sounding rocket tangent ogive noses
Author(s) -
L. D. Wing
Publication year - 1973
Publication title -
nasa sti repository (national aeronautics and space administration)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1973-281
Subject(s) - aerodynamics , sounding rocket , aerodynamic heating , aerospace engineering , tangent , rocket (weapon) , computer science , mechanics , engineering , physics , mathematics , geometry , heat transfer
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