SBIR/STTR
Innovative Aerodynamic Modeling for Aeroservoelastic Analysis and Design, Phase I
Project Introduction
We propose the development of a modern panel code for calculation of steady and unsteady aerodynamic loads needed for dynamic servoelastic (DSE) analysis of flight vehicles. The code will be especially tailored to be robust, reliable, and integrated with the NASA Object Oriented Optimization (O3) system through selection of analysis methods, file formats, and computing environment, allowing it to be efficiently applied to numerous problems of interest to NASA and industry.
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
| M4 Engineering, Inc. | Lead Organization | Industry | Long Beach, California |
Armstrong Flight Research Center
(AFRC)
|
Supporting Organization | NASA Center | Edwards, California |
| University of Washington (UW) | Supporting Organization | Academia | Seattle, Washington |
Primary U.S. Work Locations
-
California
-
Washington
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Organization:
- M4 Engineering, Inc.
Responsible Program:
- SBIR/STTR
Project Management
Program Director:
Program Manager:
Principal Investigator:
Co-Investigator:
- Myles Baker
Project Duration
Start: Jun 2015
End: Jun 2016
Technology Maturity (TRL)
| Start: | 6 |
| Current: | 6 |
| Estimated End: | 8 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TX02 Flight Computing and Avionics
- TX02.1 Avionics Component Technologies
- TX02.1.3 High Performance Processors
Target Destinations
The Sun, Earth, The Moon, Others Inside the Solar System, Outside the Solar System, Mars
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