Accession Number : AD0784883
Title : A Generalized Analysis of the Performance of a Variety of Drive Systems for High Reynolds Number, Transonic, Wind Tunnels.
Descriptive Note : Technical rept.,
Corporate Author : ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (ENGLAND)
Personal Author(s) : Pugh,P. G. ; Evans,J. Y. G.
Report Date : FEB 1974
Pagination or Media Count : 100
Abstract : Many types of wind tunnels have been proposed for transonic testing of aircraft models at high reynolds numbers. While some form of stored-energy system is needed in order to avoid exorbitant running costs, designs can vary considerably in the extent to which effective use is made of the mass of air stored in the circuit, in the energy input needed between runs, and in the quality of flow in the test section. Some of the most promising designs can be considered as variants of same thermodynamic cycle, and a generalised study has been made of their relative merits.
Descriptors : *Transonic wind tunnels, *High energy, *Cost effectiveness, *Reviews, Model tests, Aircraft, Reynolds number, Energy storage, Utilization, Great Britain, Systems engineering, Thermodynamic cycles, Drives, Performance(Engineering), Viscous flow, Mathematical models, Experimental design
Subject Categories : Test Facilities, Equipment and Methods
Distribution Statement : APPROVED FOR PUBLIC RELEASE