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Transonic Wind Tunnel Testing
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TLDR
In this article, a transsonique souffleries with a couche couche is described. Reference Record created on 2005-11-18, modified on 2016-08-08Abstract:
Keywords: transsonique ; souffleries ; couche : limite ; ecoulement ; avions ; modeles ; essais ; grille Reference Record created on 2005-11-18, modified on 2016-08-08read more
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Faculty of Mechanical Engineering
TL;DR: The Faculty of Mechanical Engineering, University of Žilina, Slovak National University as mentioned in this paper, deals with standard disciplines (such as measurement, automation, industrial engineering, technological engineering, mechanic and strength, design and machine elements) and with specific engineering disciplines such as machinery maintenance engineering; railway vehicles; engines and lifting equipment; heat and hydraulic machinery.
Journal ArticleDOI
A short history of the European Transonic Wind Tunnel ETW
John Green,Jürgen Quest +1 more
TL;DR: The European Transonic Wind Tunnel (ETW) as discussed by the authors is a transonic wind tunnel that provides transonic testing at high Reynolds numbers in a cryogenic environment, with the main purpose of testing aerodynamic properties.
Calibration of the Langley 16-foot transonic tunnel with test section air removal
TL;DR: The Langley 16-foot transonic tunnel with test section air removal (plenum suction) was calibrated to a Mach number of 1.3 in this paper, including the effects of slot shape modifications, test section wall divergence, and water vapor condensation.
Proceedings ArticleDOI
Experimental Evaluation of an Embedded Boundary Layer Ingesting Propulsor for Highly Efficient Subsonic Cruise Aircraft
David J. Arend,John D. Wolter,Stefanie M. Hirt,Andrew J. Provenza,John A. Gazzaniga,William T. Cousins,Larry W. Hardin,Sharma Om P +7 more
Journal ArticleDOI
Mitigation of wind tunnel wall interactions in subsonic cavity flows
Justin L. Wagner,Katya M. Casper,Steven J. Beresh,John F. Henfling,Russell Spillers,Brian Owen Matthew Pruett +5 more
TL;DR: In this article, a parametric approach was taken for flow over an L/D = 7 cavity at Mach numbers 0.6-0.8, and the authors found that the cavity resonance can be altered by tunnel sidewalls and that spanwise coupling should be addressed when conducting subsonic cavity experiments.