Steady and Unsteady Asymmetric Flow Regions Past an Axisymmetric Body-Reference-Cited by-同舟云学术

Steady and Unsteady Asymmetric Flow Regions Past an Axisymmetric Body

Published:2021-09 Issue:9 Volume:59 Page:3375-3386
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Jiménez-Varona José¹,Liaño Gabriel²,Castillo José L.¹,García-Ybarra Pedro L.¹

Affiliation:

1. National Distance Education University, 28040 Madrid, Spain

2. National Institute of Aerospace Technology, 28850 Madrid, Spain

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J059987

Reference18 articles.

1. ChampignyP. “High Angle of Attack Aerodynamics,” AGARD R-804 Special Course on Missile Aerodynamics, AGARD: Advisory Group for Aerospace Research and Development, June 1994, pp. 5-1–5-19.

2. LamontP. J. “The Complex Asymmetric Flow over a 3.5D Ogive Nose and Cylindrical Afterbody at High Angles of Attack,” AIAA Paper 1982-0053, 1982. 10.2514/6.1982-53

4. Asymmetric vortex forces and wakes on slender bodies

5. KruseR. L.KeenerE. R.ChapmanG. T.ClaserG. “Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 58 Degrees and Mach Numbers to 2,” NASA TM-78533, 1979.

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