Open AccessNumerical analysis of the Trailblazer inlet flowfield for hypersonic Mach numbers
Author(s) -
Christopher J. Steffen,
James R. DeBonis
Publication year - 2000
Publication title -
38th aerospace sciences meeting and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2000-889
Subject(s) - mach number , hypersonic speed , mechanics , perfect gas , mach wave , shock (circulatory) , adiabatic process , drag divergence mach number , mach reflection , aerospace engineering , computational fluid dynamics , shock tube , physics , thermodynamics , materials science , aerodynamics , shock wave , engineering , transonic , medicine
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