The design of a 3.4 by 3.4 inch supersonic wind tunnel capable of continuous operation in the range of Mach numbers between 1.50 and 3.59

Anderson, Euell Clay2016-05-232016-05-231962http://hdl.handle.net/10919/7099373 leavesapplication/pdfen-USIn CopyrightLD5655.V855 1962.A549Supersonic wind tunnels -- DesignWind tunnels -- DesignThe design of a 3.4 by 3.4 inch supersonic wind tunnel capable of continuous operation in the range of Mach numbers between 1.50 and 3.59Thesis