Near Field of an Axisymmetric Underexpanded Jet and an Adjacent Parallel Surface-Reference-Cited by-同舟云学术

Near Field of an Axisymmetric Underexpanded Jet and an Adjacent Parallel Surface

Published:2017-08 Issue:8 Volume:55 Page:2489-2502
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Hortensius Ruben¹,Dutton J. Craig¹,Elliott Gregory S.¹

Affiliation:

1. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801

Funder

Army Research Office

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.J055515

Reference37 articles.

1. RaineyR. W. “Interference Effects upon Fuselage Drag of a Jet Exhausting from a Wing-Mounted Nacelle,” NACA RM L56A09, 1955.

2. SalmiR. J.KlannJ. L. “Interference Effects at Mach 1.9 on a Horizontal Tail due to Trailing Shock Waves from an Axisymmetric Body with an Exiting Jet,” NACA RM E55J13a, 1956.

3. EnglertG. W.WasserbauerJ. F.WhalenP. “Interaction of a Jet and Flat Plate Located in an Airstream,” NACA RM E55G19, 1955.

4. WasserbauerJ. F.EnglertG. W. “Interaction of an Exhaust Jet and Elementary Contoured Surfaces Located in a Supersonic Air Stream,” NACA RM E56A16, 1956.

5. BressetteW. E. “Investigation of the Jet Effects on a Flat Surface Downstream of the Exit of a Simulated Turbojet Nacelle at a Free-Stream Mach Number of 2.02,” NACA RM L54E05a, 1954.

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