NASA SBIR 2012 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 12-2 A3.04-8924
PHASE 1 CONTRACT NUMBER: NNX13CL27P
SUBTOPIC TITLE: Aerodynamic Efficiency - Drag Reduction Technology
PROPOSAL TITLE: Energy-Deposition to Reduce Skin Friction in Supersonic Applications

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Physics, Materials, and Applied Mathematics Research, LLC
1665 E. 18th Street, Suite 112
Tucson, AZ 85719 - 6808
(520) 903-2345

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Nathan Tichenor
ntichenor@physics-math.com
200 Discovery Drive Suite 102
College Station, TX 77843 - 7546
(979) 485-9232

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Margaret Chiang
margaret.chiang@physics-math.com
1665 E. 18th Street, Suite 112
Tucson, AZ 85719 - 6808
(310) 261-2075

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 4
End: 5

Technology Available (TAV) Subtopics
Aerodynamic Efficiency - Drag Reduction Technology 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)
NASA has drawn attention to an impending need to improve energy-efficiency in low supersonic (M<~3) platforms. Aerodynamic efficiency is the foundation of energy-efficient flight in any regime, and low drag is one of the fundamental characteristics of aerodynamic efficiency. For supersonic aircraft, drag can be broadly decomposed into four components: viscous or skin friction drag, lift-induced drag, wave or compressibility drag, and excrescence drag. The relative impact of these four drag forces depends upon vehicle-specific characteristics and design. However, viscous skin friction drag stands out as particularly significant across most classes of flight vehicles. Therefore, effective techniques to reduce skin friction drag on a vehicle will have a major and far-reaching impact on flight efficiency for low supersonic aircraft. In an effort to address the need for increased aerodynamic efficiency of low supersonic vehicles, PM&AM Research, in collaboration with Texas A&M University, propose to build upon our successful Phase I effort to mature/develop our novel energy deposition technologies, using basic, well-demonstrated energy-deposition techniques along the surface in supersonic flow to control/compress/forcibly-move the boundary layer fluid by creating a low-density "bubble-like" region, thereby reducing the viscous skin friction. Once matured, this solution will reduce the drag experienced by a low supersonic platform, allowing vehicles to exhibit increased aerodynamic efficiency.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Our technology can be used to improve the aerodynamic efficiency of a wide range of supersonic NASA programs, including access to space platforms and prototype aircraft.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Our technology can be used to improve the aerodynamic efficiency of a wide range of supersonic Government and industry platforms including supersonic business jets, commercial and military access to space vehicles, supersonic cruise vehicles, and high-speed delivery platforms, among others

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.)
Active Systems
Actuators & Motors
Aerodynamics
Atmospheric Propulsion
Circuits (including ICs; for specific applications, see e.g., Communications, Networking & Signal Transport; Control & Monitoring, Sensors)
Conversion
Lasers (Weapons)
Models & Simulations (see also Testing & Evaluation)
Transport/Traffic Control
Vehicles (see also Autonomous Systems)

Form Generated on 03-04-14 13:38