Trail left by missiles and satellites in hypersonic flow is divided into expansion controlled and conduction controlled trail; times required for ionization and dissociation to go to completion, are important in determining observable effects of trails, i.e., emitted thermal radiation and reflection of electromagnetic waves; computational procedure for behavior of conduction controlled trail is developed based on integral methods.
On trials of axisymmetric hypersonic blunt bodies flying through atmosphere
J Aerospace Sciences
Journal of Aerospace Sciences ; 28 , n 6
1961
Aufsatz (Zeitschrift)
Englisch
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Augmented Burnett-Equation Solutions over Axisymmetric Blunt Bodies in Hypersonic Flow
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