← Back to NASA Technology Projects
Probabilistic Formulation of Multi-fidelity Aerodynamic Databases (ProForMA)
Completed
TRL 5 (started at 2, targeting 5)
Description
The design of new aircraft involves understanding the flow physics around the configurations as well as their stability and control characteristics over the entire flight envelope. Such a coverage is extremely expensive if wind tunnel and flight tests are the primary means of understanding the aerodynamic characteristics. Hence, there has been a push towards use of simulations for understanding aerodynamics of airframes early in the design process. However, high-fidelity simulations can quickly become very expensive, so there is a need to create multi-fidelity databases for aerodynamic data. For this purpose, IAI proposes to develop probabilistic aerodynamic databases, that not only provide confidence on the fit, but also characterize the sources of uncertainty. Morever, adaptive design of experiments are performed for maximum efficiency in database creation. The proposed ProForMA tool can fill in a critical gap in design optimization and certification tools used by NASA and the industry
Benefits
ProForMA addresses a critical need in NASA’s repository of tools and techniques to develop unconventional aircraft. Several T&E efforts at NASA, have to bear exorbitant costs for fully testing new concepts. The proposed approach contributes to the state-of-the-art in T&E taking advantage of latest advances in HPC to alleviate costs. Benefits of this tool can be leveraged by all programs concerned with unconventional aircraft, such as AAVP, TACP, MUTT and ASE
Other government agencies, interested in unconventional aircraft, such as the Air Force, may use this tool for programs such as N-MAS and AAW or to reduce costs of T&E (AF T&E program). Navy’s UCLASS program also stands to benefit from this. Boeing is already quite interested in this research and envisions a huge potential for ProForMA in understanding stability and control characteristics of new aircraft
Details
| Technology area | Flight Vehicle Systems > Aeroscience > Aeroelasticity |
| Program | Small Business Innovation Research/Small Business Tech Transfer (SBIR/STTR) |
| Lead organization | Intelligent Automation, Inc., Rockville, MD |
| Start date | 2018-07-27 |
| End date | 2019-02-15 |
Project contacts
Listed on TechPort itself — the most direct way to ask about this specific project.
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.
None of these are guaranteed paths for this specific project — TechPort itself doesn't have an "apply" button. Reaching out to the contact(s) above with a specific question is usually the fastest way to find out what's actually open.