Particle image velocimetry in Mach 3.5 and 4.5 shock-tunnel flows

AIAA Journal

Volumn 40, Issue 6, 2002, Pages 1056-1060

  Haertig, J ^a   Havermann, M ^a   Rey, C ^a   George, A ^a  

^a FRENCH GERMAN RESEARCH INSTITUTE OF SAINT LOUIS   (France)

Author keywords

[No Author keywords available]

Indexed keywords

IMAGING TECHNIQUES; NOZZLES; SHOCK TUBES; SUPERSONIC FLOW; VELOCITY MEASUREMENT; WIND TUNNELS;

PARTICLE IMAGE VELOCIMETRY; SHOCK TUNNEL;

AERODYNAMICS;

EID: 0036602745     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1787     Document Type: Article

References (13)

1. Introduction
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6. PIV measurements in sub- and supersonic flow over the delta wing configuration ELAC
7. Investigation of the supersonic flow field around a delta wing using particle image velocimetry
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9. Underexpanded sonic jets: A PIV study
10. Stereoscopic PIV measurements of a screeching supersonic jet
11. Anemométrie Laser, Amélioration de la Précision des Mesures par Élimination des Erreurs dues à la Présence de Grosses Particules
12. TRUE resolution PIV: A mesh-free second order-accurate algorithm