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Dhawan, Satish (1949-01-01) On the design and use of a flexible nozzle for the Galcit tronsonic tunnel. http://resolver.caltech.edu/CaltechETD:etd-04202004-110634


Type of Document Engineer's Thesis
Author Dhawan, Satish
URN etd-04202004-110634
Persistent URL http://resolver.caltech.edu/CaltechETD:etd-04202004-110634
Title On the design and use of a flexible nozzle for the Galcit tronsonic tunnel
Degree Engineer's Degree
Option Aeronautics
Advisory Committee
Advisor Name Title
Hans Wolfgang Liepmann Committee Chair
Keywords
  • none
Date of Defense 1949-01-01
Availability unrestricted
Abstract
Some aspects concerning the design of flexible nozzles for use in supersonic wind tunnels are discussed. Methods are investigated for matching the deflection patterns of nozzle plates and the theoretical aerodynamic shapes required for uniform, parallel, shockfree flow. Application of the design procedures to the Galcit 4" x 10", transonic wind tunnel is detailed. As a demonstration of a use of the tunnel, the Mach number of shock detachment from a 10[degree] wedge (half angle) is experimentally investigated.
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