Abstract
Experimental results in transonic, highly separated turbulent flow are presented. The model is an air intake of 20 × 80 mm2 section set with an angle of attack from 20 to 40° inside a M = 0.7 free jet flow. The Mach numbers and mass flow rates are deduced from pressure measurements. Flow visualization, laser-Doppler and hot wire anemometers are used to analyse the mean velocity field, unsteadiness and turbulent flow characteristics.
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References
Leblanc, R., Thiebault, P., Ardonceau, P., Goethals, R.: “Etude expérimentale des entrées d’air transoniques aux grandes incidences”, Final Report, Contrat DRET 77/214 (1978)
Thiebault, P., Ardonceau, P., Leblanc, R., Goethals, R.: First measurements in highly separated transonic flow. Mech. Res. Commun. 6, 113–114 (1979)
Ardonceau, P.: “Application de l’anémométrie laser à l’aérodynamique supersonique”, Thèse de 3ième Cycle, University of Poitiers (1974)
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© 1982 Springer-Verlag Berlin Heidelberg
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Farcy, A., Mercier, V., Leblanc, R. (1982). Experimental Investigations in Transonic Highly Separated, Turbulent Flow. In: Bradbury, L.J.S., Durst, F., Launder, B.E., Schmidt, F.W., Whitelaw, J.H. (eds) Turbulent Shear Flows 3. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-95410-8_18
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DOI: https://doi.org/10.1007/978-3-642-95410-8_18
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-95412-2
Online ISBN: 978-3-642-95410-8
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