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Inviscid Store Separation During Transonic Flight With Deployable Fins Using (6+) DOF

[+] Author Affiliations
Jonathan G. Dudley

Sentel, Inc., Eglin AFB, FL

William Westmoreland

Sverdrup Technology, Inc., Eglin AFB, FL

Paper No. PVP2004-3142, pp. 251-259; 9 pages
doi:10.1115/PVP2004-3142
From:
  • ASME/JSME 2004 Pressure Vessels and Piping Conference
  • Computational Technologies for Fluid/Thermal/Structural/Chemical Systems With Industrial Applications, Volume 2
  • San Diego, California, USA, July 25–29, 2004
  • Conference Sponsors: Pressure Vessels and Piping Division
  • ISBN: 0-7918-4686-5
  • Copyright © 2004 by ASME

abstract

The classical rigid body 6 DOF capability at Eglin AFB has been completely rewritten. The new (6+) DOF allows moving components relative to non-inertial reference frames during time accurate CFD simulations. An inviscid computational fluid dynamics model was prepared to investigate the separation of a 2,000 lb cluster munition (CBU104) with deployable fins from an F15-E at transonic speed using (6+) DOF. The Mach effects of the store with deployable fins were studied for a given fighter aircraft configuration prior to USAF flight clearance.

Copyright © 2004 by ASME

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