Experimental Investigations on the Phantom Yaw Effect on a Maneuvering Slender Body-Reference-Cited by-同舟云学术

Experimental Investigations on the Phantom Yaw Effect on a Maneuvering Slender Body

Published:2015-01 Issue:1 Volume:52 Page:264-274
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Wysocki Oliver¹,Schülein Erich¹

Affiliation:

1. Institute of Aerodynamics and Flow Technology, DLR, German Aerospace Center, 37073 Göttingen, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A32885

Reference17 articles.

1. FiechterM. “Über Wirbelsysteme an schlanken Rotationskörpern und ihren Einfluss auf die aerodynamischen Beiwerte,” German–French Research Inst. of Saint-Louis, TR-10/66, Saint-Louis, France, 1966.

2. Asymmetric vortex forces and wakes on slender bodies

3. Wind-tunnel studies on maneuvering slender bodies

4. Closed-Loop Missile Yaw Control via Manipulation of Forebody Flow Asymmetrics

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3. The lateral force hysteretic characteristic of a pitching slender body without and with synthetic jet control;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-05-08