Heat-transfer measurements boundary-layer transition, and the effects of superpolishing observed in two free-flight tests up to Mach number 5.0 at Reynolds number per foot up to 8 x 106

Hall, James Rudyard2015-06-262015-06-261961http://hdl.handle.net/10919/5380593 leavesapplication/pdfen-USIn CopyrightLD5655.V855 1961.H34Heat -- TransmissionBoundary layerAirplanes -- Flight testingHeat-transfer measurements boundary-layer transition, and the effects of superpolishing observed in two free-flight tests up to Mach number 5.0 at Reynolds number per foot up to 8 x 106Thesis