Electrodynamic control of shock interactions in a 25°/55° double cone model in hypersonic flow

Katsumi Wasai, Hitoshi Makino, Yasunori Nagata, Katsumi Hiraoka, Kazuhiko Yamada, Takashi Abe

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Citations (Scopus)

Abstract

The numerical simulation for the magnetic interaction in the hypersonic flow around the double cone model predicts that as a result of the interaction, the shock wave generated by the second cone is primarily affected and is shifted away from the model surface, affecting the separation bubble. Furthermore, because of this interaction, the separation bubble is enhanced. To validate the numerical prediction, we have conducted an experimental investigation by mean of the expansion tube facility which enables us to generate a high speed flow of 12 km/sec. For measurement, the sequential images of the flow around a model were recorded. The experimental result agrees with the numerical prediction at least qualitatively. As a matter of fact, in the experiment, we can observe the effect of the applied magnetic field more clearly than expected. The flow control accomplished by the present magnetic interaction is qualitatively equivalent to the one accomplished by the increase of the half-angle of the second cone which may represent the aerodynamic control surface. In this context, the present magnetic interaction may have a possibility to replace the mechanical aerodynamic control surface.

Original languageEnglish
Title of host publication48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
Publication statusPublished - 2010
Externally publishedYes
Event48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition - Orlando, FL, United States
Duration: Jan 4 2010Jan 7 2010

Other

Other48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
CountryUnited States
CityOrlando, FL
Period1/4/101/7/10

Fingerprint

Hypersonic flow
Electrodynamics
Cones
Control surfaces
Aerodynamics
Flow control
Shock waves
Magnetic fields
Computer simulation
Experiments

ASJC Scopus subject areas

  • Aerospace Engineering

Cite this

Wasai, K., Makino, H., Nagata, Y., Hiraoka, K., Yamada, K., & Abe, T. (2010). Electrodynamic control of shock interactions in a 25°/55° double cone model in hypersonic flow. In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition [2010-0257]

Electrodynamic control of shock interactions in a 25°/55° double cone model in hypersonic flow. / Wasai, Katsumi; Makino, Hitoshi; Nagata, Yasunori; Hiraoka, Katsumi; Yamada, Kazuhiko; Abe, Takashi.

48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010. 2010-0257.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Wasai, K, Makino, H, Nagata, Y, Hiraoka, K, Yamada, K & Abe, T 2010, Electrodynamic control of shock interactions in a 25°/55° double cone model in hypersonic flow. in 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition., 2010-0257, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, FL, United States, 1/4/10.
Wasai K, Makino H, Nagata Y, Hiraoka K, Yamada K, Abe T. Electrodynamic control of shock interactions in a 25°/55° double cone model in hypersonic flow. In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010. 2010-0257
Wasai, Katsumi ; Makino, Hitoshi ; Nagata, Yasunori ; Hiraoka, Katsumi ; Yamada, Kazuhiko ; Abe, Takashi. / Electrodynamic control of shock interactions in a 25°/55° double cone model in hypersonic flow. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010.
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