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

Description

Master of Science

Links & Downloads

1. http://hdl.handle.net/10919/53805

Tags

LD5655.V855 1961.H34

Heat -- Transmission

Boundary layer

Airplanes -- Flight testing

Additional Fields

Identifer	oai:union.ndltd.org:VTETD/oai:vtechworks.lib.vt.edu:10919/53805
Date	January 1961
Creators	Hall, James Rudyard
Contributors	Aerospace Engineering
Publisher	Virginia Polytechnic Institute
Source Sets	Virginia Tech Theses and Dissertation
Language	en_US
Detected Language	English
Type	Thesis, Text
Format	93 leaves, application/pdf, application/pdf
Rights	In Copyright, http://rightsstatements.org/vocab/InC/1.0/
Relation	OCLC# 20188818