30th Aerospace Sciences Meeting and Exhibit 1992
DOI: 10.2514/6.1992-254
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Integrated numerical methods for hypersonic aircraft cooling systemsanalysis

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Cited by 3 publications
(2 citation statements)
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“…8) Assess key stability issues if they appear to be significant design drivers, e.g., aeroelasticity, propellant sloshing in tanks, pogo, etc. ; and b) use load indicators.…”
Section: Conceptual Design Phasementioning
confidence: 99%
“…8) Assess key stability issues if they appear to be significant design drivers, e.g., aeroelasticity, propellant sloshing in tanks, pogo, etc. ; and b) use load indicators.…”
Section: Conceptual Design Phasementioning
confidence: 99%
“…Generally it is known a priori that the engine flowpath requires active cooling. 7 The upper left-hand corner of Figure 12 shows an example of a coolant routing along the keel-line of the inlet, combustor and nozzle. Schematically, the active cooling network is shown in the middle of the figure.…”
Section: Thermal Managementmentioning
confidence: 99%