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Energy-Deposition to Reduce Skin Friction in Supersonic Applications
Completed
TRL 5 (started at 3, targeting 5)
Description
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 demonstrate the feasibility of depositing energy using basic, well-demonstrated 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. If successful, this solution will reduce the drag experienced by a low supersonic platform, allowing vehicles to exhibit increased aerodynamic efficiency.
Benefits
Our technology could be used to improve the aerodynamic efficiency of a wide range of supersonic NASA programs, including access to space platforms and prototype aircraft.
Our technology could be used to improve the aerodynamic efficiency of a wide range of supersonic Government and industry platforms including commercial and military access to space vehicles, supersonic cruise vehicles, and high-speed delivery platforms, among others.
Details
| Technology area | Flight Vehicle Systems > Aeroscience > Aerodynamics |
| Program | Small Business Innovation Research/Small Business Tech Transfer (SBIR/STTR) |
| Lead organization | Physics, Materials, and Applied Mathematics Research, LLC, Tucson, AZ |
| Start date | 2013-05-23 |
| End date | 2013-11-23 |
Project contacts
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How to get involved
This is early/mid-stage (TRL 5) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.
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