Rear stagnation point location in a subsonic near-wake-Reference-Cited by-同舟云学术

Rear stagnation point location in a subsonic near-wake

Published:1976-05 Issue:5 Volume:13 Page:319-320
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Merz R. A.¹,Page R. H.²,Przirembel C. E. G.²

Affiliation:

1. Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio

2. Rutgers University, New Brunswick N.J.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.27911

Reference5 articles.

1. !Merz, R.A. "The Turbulent Near-Wake of an Axisymmetric Blunt Based Body at Subsonic Speeds," Ph.D. Thesis, Mechanical,Industrialand Aerospace Engineering Department,Rutgers University, New Brunswick, N.J.May 1975.

2. 2McErlean, D.P. "The Near-Wake of a Blunt Based Axisymmetric Body at Mach 0.14," Ph.D. Thesis, Mechanical,Industrialand Aerospace Engineering Department,Rutgers University, New Brunswick, N.J.Jan. 1970.

3. 3Przirembel, C.E.G. "The Turbulent Near-Wake of an Axisymmetric Body at Supersonic Speeds," Ph.D. Thesis, Mechanical,Irfdustrialand Aerospace Engineering Department,Rutgers University, New Brunswick, N.J.June 1967.

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