NASA STTR 2015 Solicitation

FORM 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.)
Aerodynamics
Autonomous Control (see also Control & Monitoring)
Models & Simulations (see also Testing & Evaluation)
Software Tools (Analysis, Design)
Structures

Form Generated on 08-29-16 14:51