1955
DOI: 10.21236/ad0075320
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A Theoretical Investigation of Turbulent Boundary Layer Flow With Heat Transfer at Supersonic and Hypersonic Speeds

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Cited by 8 publications
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“…(ID Approximations (9) and (10) imply that the length of the interaction is small (or constant) relative to distance from the effective origin of the boundary layer. That is, the change in boundary layer edge slope and T /p due to the natural boundary layer growth (without a shock wave impingement) must be small compared to the changes imposed by the sudden pressure rise.…”
Section: Interaction Correlationmentioning
confidence: 99%
“…(ID Approximations (9) and (10) imply that the length of the interaction is small (or constant) relative to distance from the effective origin of the boundary layer. That is, the change in boundary layer edge slope and T /p due to the natural boundary layer growth (without a shock wave impingement) must be small compared to the changes imposed by the sudden pressure rise.…”
Section: Interaction Correlationmentioning
confidence: 99%