Increase in stagnation pressure and enthalpy in shock tunnelsA new technique based on the insertion of a converging section in the driven tube is described which is capable of producing substantial increases in both reservoir pressure and enthalpy. A 1D inviscid full kinetics code is used to study a number of different locations and shapes for the converging driven tube section. For driven tube diameter reductions of factors of 2 and 3, the reservoir pressure is found to increase by factors of 2.1 and 3.2, respectively, and the enthalpy is found to simultaneously increase by factors of 1.5 and 2.1, respectively.
Document ID
19930039038
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bogdanoff, David W. (NASA Ames Research Center Moffett Field, CA, United States)
Cambier, Jean-Luc (Eloret Inst. Palo Alto, CA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 93-0350Report Number: AIAA PAPER 93-0350
Meeting Information
Meeting: AIAA, Aerospace Sciences Meeting and Exhibit