Rotorcraft Brownout Aerodynamic Analysis and Flight Simulation

Award Information
Agency: Department of Defense
Branch: Army
Contract: W911W6-05-C-0033
Agency Tracking Number: A043-085-1102
Amount: $119,663.00
Phase: Phase I
Program: SBIR
Awards Year: 2005
Solicitation Year: 2004
Solicitation Topic Code: A04-085
Solicitation Number: 2004.3
Small Business Information
CONTINUUM DYNAMICS, INC.
34 Lexington Avenue, Ewing, NJ, 08618
DUNS: 096857313
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Daniel Wachspress
 Associate
 (609) 538-0444
 dan@continuum-dynamics.com
Business Contact
 Barbara Agans
Title: Adminstrator
Phone: (609) 538-0444
Email: barbara@continuum-dynamics.com
Research Institution
N/A
Abstract
A critical operational problem for current Army rotorcraft is the prediction of landing conditions in a sand/dust/snow laden environment where rotorwash picks up loose ground cover leading to a condition of obscured visibility known as "brownout". The proposed effort will develop both a comprehensive analysis and flight simulation tool able to predict the magnitude and distribution of visibility difficulties associated with brownout. An accelerated timetable is projected by integrating and enhancing several state-of-the-art technologies already in place at Continuum Dynamics, Inc. (CDI). These technologies include: CDI's CHARM full-span free-vortex wake model and fast panel fuselage/ground surface model for general rotorcraft flow fields in steady and transient flight including a real-time free wake option for flight simulation applications; CDI's Army-accredited LDTRAN/CB model of particle uptake, entrainment and transport; an enhanced version of the Army's GenHel flight simulation software; and CDI's VRML/X3D out-the-window display technology that already supports the rendering of visual obscuration. Building quickly on these validated technologies, it is expected that a prototype rotorcraft brownout analysis and flight simulation tool can be completed in Phase I, followed by a significant expansion of features, validation and packaging in Phase II including a real-time flight simulation capability.

* information listed above is at the time of submission.

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