Mitigation of Supersonic Aircraft Pod Aero-Optics

Award Information
Agency: Department of Defense
Branch: Defense Advanced Research Projects Agency
Contract: W31P4Q-17-C-0127
Agency Tracking Number: D2-1861
Amount: $1,748,449.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: AF103-001
Solicitation Number: 2010.3
Timeline
Solicitation Year: 2010
Award Year: 2018
Award Start Date (Proposal Award Date): 2017-08-29
Award End Date (Contract End Date): 2019-11-29
Small Business Information
2021 Girard Blvd. SE, Suite 150, Albuquerque, NM, 87106
DUNS: 794350025
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Dr. Matthew Whiteley
 (937) 684-4100
 matthew.whiteley@mza.com
Business Contact
 Robert Praus
Phone: (505) 459-9970
Email: contracts@mza.com
Research Institution
N/A
Abstract
A technical plan is proposed for developing a supersonic pod-based application of virtual duct passive flow control for aero-optic mitigation. Virtual ducts have proven to be a highly effective tool for achieving aero-optic mitigation transonic flight up to Mach 0.8, and the proposed work seeks to leverage our extensive experience in designing and testing transonic virtual ducts to develop a unified fairing architecture that will yield effective aero-mitigation continuously across both the transonic and supersonic regimes. Supersonic virtual duct fairing (VDF) designs will be evaluated using CFD to optimize the VDF shape. We will also construct a subscale optical model to facilitate wind tunnel testing of our supersonic fairing design. Preliminary testing will be performed in university wind tunnel facilities, and an entry into a government wind tunnel facility is proposed for a thorough evaluation of VDF performance at a range of Mach numbers and viewing angles. CFD generated wavefront and pressure data will also be used as a basis for the design of a beam control system which will complement passive aero-mitigation with the VDF in order to achieve weapons-quality system optical performance for the supersonic flight regime.

* Information listed above is at the time of submission. *

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