A Turbulent Boundary Layer with Mass Addition, Combustion, and Pressure Gradients-Reference-Cited by-同舟云学术

A Turbulent Boundary Layer with Mass Addition, Combustion, and Pressure Gradients

Published:1971-09 Issue:9 Volume:9 Page:1762-1768
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

JONES J. W.¹,ISAACSON L. K.²,VREEKE S.²

Affiliation:

1. The Ohio State University, Columbus, Ohio

2. University of Utah, Salt Lake City Utah

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.49978

Reference18 articles.

1. Jones, J. W.j "A Turbulent Boundary Layer with Mass Addition, Combustion, and Pressure Gradients," Ph.D. dissertation,April 1970, Dept. of Mechanical Engineering,Univ. of Utah, Salt Lake City, Utah.

2. Measurements in a turbulent boundary layer with porous wall injection and combustion

3. Transport processes in a combustible turbulent boundary layer

4. Smith, T. H. "Hot-Film Characteristics in a Turbulent Boundary Layer with Foreign-Gas Injection," Ph.D. dissertation,June 1969, Dept. of Mechanical Engineering,Univ. of Utah, Salt Lake City, Utah.

5. Laminar boundary-layer wedge flows with evaporation and combustion

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