Laminar Compressible Mixing Behind Finite Bases.
ResearchPublished 1963
Because of the recent interest in the fluid-mechanic description of hypersonic wakes, laminar mixing problems are again being investigated both experimentally and theoretically. This paper shows that the velocity along the dividing streamline can be determined in a simple manner by approximating the integral solution contained in NACA Report 958, "Laminar Mixing of a Compressible Fluid," by D. R. Chapman. The effect of finite base radius (or Reynolds number) is also investigated using this approximate solution. 7 pp.
Document Details
- Copyright: RAND Corporation
- Availability: Available
- Year: 1963
- Print Format: Paperback
- Paperback Pages: 7
- Paperback Price: $20.00
- Document Number: P-2828
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Lykoudis, P. S., Laminar Compressible Mixing Behind Finite Bases. RAND Corporation, P-2828, 1963. As of September 23, 2024: https://www.rand.org/pubs/papers/P2828.html
Lykoudis, P. S., Laminar Compressible Mixing Behind Finite Bases. Santa Monica, CA: RAND Corporation, 1963. https://www.rand.org/pubs/papers/P2828.html. Also available in print form.
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