Behaviour of turbulent Prandtl/Schmidt number in compressible mixing layer
Author:
Affiliation:
1. Directorate of Computational Dynamics, Defence Research and Development Laboratory, Kanchanbagh, Hyderabad, India
2. Department of Aerospace Engineering, Indian Institute of Science, Bangalore, India
Abstract
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/0954410014547441
Reference19 articles.
1. Heat and Mass Transport
2. The variation of turbulent Prandtl and Schmidt numbers in wakes and jets
3. Turbulent Prandtl Number—Where Are We?
4. Analysis of Supersonic Combustors with Swept Ramp Injectors
5. Analysis of Dual-Mode Hydrocarbon Scramjet Operation at Mach 4-6.5
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