Heat transfer from a simulated shuttle external tank in the naturally turbulent outdoor environmentTo estimate the local heat-transfer coefficients around an external-tank (ET) surface, a 9.8-m-high by 8.4-m-diameter ET simulator is constructed, instrumented, and tested in the naturally turbulent outdoor environment. Two different configurations under which the testing is conducted are described. The time-average, local values of Nusselt number at time-average Reynolds numbers of 2.2 x 10 to the 6th, 2.6 x 10 to the 6th, and 4.5 x 10 to the 6th are presented. It is shown that, at the same Reynolds numbers, the heat transfer coefficients due to the atmospheric airflow are higher than those due to airflow in a low-turbulent-intensity wind tunnel.
Document ID
19850055495
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lin, F. N. (NASA John F. Kennedy Space Center Cocoa Beach, FL, United States)
Littlefield, M. D. (NASA Kennedy Space Center FL, United States)