DocumentCode :
1410064
Title :
Instrumentation of a Pilot Counterflow Facility
Author :
Harris, Howard G.
Author_Institution :
von Kármán Gas Dynamics Facility, ARO, Incorporated, Arnold Air Force Station, Tenn.
Issue :
3
fYear :
1967
fDate :
5/1/1967 12:00:00 AM
Firstpage :
424
Lastpage :
432
Abstract :
In the VKF Counterflow Facility a small test model is launched upstream through the test section flow of a shock tunnel, thus producing relative velocities greater than that of either single component. This facility is presently capable of simulating model velocities greater than 30 000 ft/s (9.2 km/s) and altitudes from 50 000 to 200 000 ft (15.2 to 61 km). Instrumentation systems and components essential to the operation of this facility are described in this paper.
Keywords :
Aerodynamics; Combustion; Electric shock; Helium; Instruments; Predictive models; System testing; Transducers; Transistors; Vehicle dynamics; Counterflow; facility; instrumentation; shock; systems; tunnel;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.1967.5408806
Filename :
5408806
Link To Document :
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