Thermophysics and Thermal ControlRaymond Viskanta |
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Page 193
... evaluated a candidate successor to the X - 15 which has been designated the X - 24C . This aircraft is a lifting body design capable of sustained operations at Mach 6. The present paper discusses the aerodynamic heating environment ...
... evaluated a candidate successor to the X - 15 which has been designated the X - 24C . This aircraft is a lifting body design capable of sustained operations at Mach 6. The present paper discusses the aerodynamic heating environment ...
Page 199
... evaluate the heating rate from equations that are based on simplified two - dimensional techniques . Determination of ... evaluated independently as a flat plate at angle of attack to the freestream velocity vector . The NSWC code is a ...
... evaluate the heating rate from equations that are based on simplified two - dimensional techniques . Determination of ... evaluated independently as a flat plate at angle of attack to the freestream velocity vector . The NSWC code is a ...
Page 206
... evaluated . These data points are shown in Fig . 13. Both static pressure data and temperature - time data were taken at each of these stations . As From the geometry of the problem , the local impact angle of the strake lower surface ...
... evaluated . These data points are shown in Fig . 13. Both static pressure data and temperature - time data were taken at each of these stations . As From the geometry of the problem , the local impact angle of the strake lower surface ...
Contents
Thermal Radiative Properties of Solar Sail Film Materials | 3 |
Infrared Reflectance and Refractive Index of Condensed Gas Films | 22 |
FarInfrared Properties of Baffle Coating Materials | 39 |
Copyright | |
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AIAA aluminum analysis angle of attack Astronautics black epoxy paint blanket boundary calorimeter coating coefficient configuration constriction resistance contact area convection cooled correlation cryodeposits cryogen deposit thickness detector determined developed dimensionless dissimilar metal distribution emittance Engineering epoxy equation evaluated experimental film flight frit groove heat flow heat flux heat leak heat loss Heat Transfer heat-transfer heater increase insulation system integral integrating sphere Kapton laser load material MAWD measured microcontacts microsphere MLI system multilayer insulation NASA nodes obtained orbit parameters predicted presented pressure radiation radiative ratio refraction refractive index REYNOLDS ANALOGY sail sample shield shown in Fig solar absorptance solar sail solid Space spacecraft spectral reflectance sphere stainless steel substrate surface Table tank temperature thermal conductivity thermal contact conductance thermal control thermal performance thermocouples Thermophysics tion titania vacuum values view angle wall wavelength ZIRCALOY