NASA STTR 2015 SolicitationFORM B - PROPOSAL SUMMARY |
| PROPOSAL NUMBER: | 15-2 T4.01-9910 |
| PHASE 1 CONTRACT NUMBER: | NNX15CD25P |
| RESEARCH SUBTOPIC TITLE: | Dynamic Servoelastic (DSE) Network Control, Modeling and Optimization |
| PROPOSAL TITLE: | Innovative Aerodynamic Modeling for Aeroservoelastic Analysis and Design |
| SMALL BUSINESS CONCERN (SBC): | RESEARCH INSTITUTION (RI): | ||
| NAME: | M4 Engineering, Inc. | NAME: | University of Washington |
| STREET: | 4020 Long Beach Boulevard | STREET: | 4333 Brooklyn Avenue Northeast, P.O. Box 359472 |
| CITY: | Long Beach | CITY: | Seattle |
| STATE/ZIP: | CA 90807 - 2683 | STATE/ZIP: | WA 98195 - 9472 |
| PHONE: | (562) 981-7797 | PHONE: | (206) 543-4043 |
PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Myles Baker
mbaker@m4-engineering.com
4020 Long Beach Boulevard
Long Beach, CA 90807 - 2683
(562) 305-3391
CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Myles Baker
mbaker@m4-engineering.com
4020 Long Beach Boulevard
Long Beach, CA 90807 - 2683
(562) 305-3391
Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 5
End: 7
Technology Available (TAV) Subtopics
Dynamic Servoelastic (DSE) Network Control, Modeling and Optimization is a Technology Available (TAV) subtopic
that includes NASA Intellectual Property (IP). Do you plan to use
the NASA IP under the award?
No
TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
We propose the development of a novel aerodynamic modeling approach making use of fully unstructured grids for unsteady panel aerodynamic models for aeroelastic and aeroservoelastic analysis. The unsteady aerodynamic code will be integrated with an existing suite of aeroelastic and aeroservoelastic analysis tools making it possible to perform aeroelastic and aeroservoelastic analysis of complex vehicles with a significant reduction in user effort and improvement in fidelity.
POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Applicable to all subsonic and supersonic aircraft applications with aeroelastic or aeroservoelastic challenges.
POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Applicable to all subsonic and supersonic aircraft applications with aeroelastic or aeroservoelastic challenges.
TECHNOLOGY TAXONOMY MAPPING (NASA's technology taxonomy has been developed by the SBIR-STTR program to disseminate awareness of proposed and awarded R/R&D in the agency. It is a listing of over 100 technologies, sorted into broad categories, of interest to NASA.)
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Aerodynamics
Autonomous Control (see also Control & Monitoring) Models & Simulations (see also Testing & Evaluation) Software Tools (Analysis, Design) Structures |