Measurement of heat transfer on a flat plate-step model at Mach 14: (Task 3.4--shock tunnel experiments--REST Project)

Sandborn, Virgil A., authorHeron K., authorResearch and Advanced Development Divison, AVCO Corp., publisher2019-09-172019-09-171963-06https://hdl.handle.net/10217/198008CER63VAS80.26 June 1963.Prepared for Air Force Ballistic Systems Division, Air Force Systems Command, United States Air Force, Norton Air Force Base, California.Includes bibliographical references.technical reportsengCopyright and other restrictions may apply. User is responsible for compliance with all applicable laws. For information about copyright law, please see https://libguides.colostate.edu/copyright.Fluid mechanicsHeat -- TransmissionHypersonic wind tunnelsMeasurement of heat transfer on a flat plate-step model at Mach 14: (Task 3.4--shock tunnel experiments--REST Project)Text