Flying-hot-wire study of two-dimensional mean flow past an NACA 4412airfoil at maximum lift-Reference-Cited by-同舟云学术

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Flying-hot-wire study of two-dimensional mean flow past an NACA 4412airfoil at maximum lift

Published:1978-07-10 Issue: Volume: Page:
ISSN:
Container-title:11th Fluid and PlasmaDynamics Conference
language:
Short-container-title:

Author:

COLES D.¹,WADCOCK A.¹

Affiliation:

1. California Institute of Technology, Pasadena, Calif.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1978-1196

Reference10 articles.

1. "CCW". Coles, D., Cantwell, B. and Wadcock, A. The flying hot wire and related instrumentation. Techn. Rep. to NASA Ames Research m r (NASA Grant NGL 05-002-229). 1977.

2. Wadcock, A. J, Flying-hot-wire study of hvodimensional turbulent separation on an NACA 4412 airfoil at maximum lift. Ph.D. Thesis, Calif. Inst.Technology, 1978.

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1. Implementation of a PAFV turbulence model for airfoil flow simulation on OpenFOAM;Physica Scripta;2024-03-29

2. Measurement and interpretation of space-time correlation functions and derivative statistics from a rotating hot wire in a grid turbulence;Experiments in Fluids;1989-06

3. Flying hot-wire anemometry;Experiments in Fluids;1984-03

4. Flying-hot-wire study of two-dimensional mean flow past an NACA 4412airfoil at maximum lift;11th Fluid and PlasmaDynamics Conference;1978-07-10

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