CFD-Based Multidisciplinary Analysis for Flight Vehicle Simulation and Control

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$100,000.00
Award Year:
2003
Program:
STTR
Phase:
Phase I
Contract:
NAS4-03013
Award Id:
61680
Agency Tracking Number:
020026
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
670 Silver Spur Rd. Suite 209, Rolling Hills Estates, CA, 90274
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
Andrew Arena
() -
aarena@okstate.edu
Business Contact:
Maj Mirmirani
Business Official
(310) 704-7490
aes_co@cox.net
Research Institute:
Oklahoma State University
Joseph Alexander
218 Engineering North
Stillwater, OK, 74078
(405) 744-6501
Nonprofit college or university
Abstract
The ability to quickly estimate flight vehicle behavior in an operational environment is particularly important since engineers from a variety of disciplines require accurate predictions in order to plan flight test experiments, expand aircraft operating envelopes safely, and have access to diagnostic methods when problems arise. In order to minimize risks, and to maximize compatibility with present NASA efforts and personnel, the innovative software to be created and marketed through this effort will be written to ?seamlessly? interface with the NASA STARS suite of codes. This approach will also allow a focus on the new and innovative techniques to be implemented during this effort without the need to reproduce analysis tools which are already highly developed and validated. At the same time, this increases commercial viability of the product due to the broad distribution and familiarity with the STARS codes in the government and academic sectors. The products ultimately produced from this effort will have the capability for CFD-based multi-disciplinary analysis of flight vehicles including linear and non-linear aeroservoelastic analysis. Special emphasis will be placed on developing tools which may be used by engineers in a flight test environment where rapid turnaround times are critical.

* information listed above is at the time of submission.

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