Opportunity Information: Apply for USAFA BAA 2015 CALL 0005
The Hypersonic Turbulence Models Research opportunity (USAFA BAA 2015 CALL 0005) is a Department of Defense effort run through the U.S. Air Force Academy to solicit unclassified research white papers, with full proposals invited later if requested. Submissions are expected to avoid proprietary content; if an applicant does include proprietary material, the burden is on the submitter to clearly mark those sections according to the instructions in USAFA-BAA-2015 Amendment 0003. The call is positioned as a research and development grant/cooperative agreement/contract pathway, meaning the government is open to funding work under multiple instrument types depending on the project and negotiations.
At its core, the call sits under the Hypersonic Vehicle Simulation Institute (HVSI), which supports the DoD High Performance Computing Modernization Program (HPCMP). The main motivation is to significantly improve the realism, reliability, and usefulness of computational simulations for hypersonic vehicles. HPCMP is focused on accelerating progress in both high-performance computing software and hardware so the DoD can model hypersonic systems more effectively during research, design, and acquisition. In practical terms, the government is looking for work that helps move hypersonic simulation beyond isolated research codes and toward robust, production-quality capabilities that can be used by government teams and their academic and industry partners.
The scope is broad but clearly centered on computational simulation advances for hypersonic flight. The opportunity highlights improvements to numerical methods, physics and engineering models, and end-to-end simulation approaches that capture key aerothermodynamic and propulsion phenomena. While the title emphasizes turbulence models, the listed technical areas show that the government is interested in coupled, high-fidelity modeling across the hypersonic environment, including turbulence, boundary layer transition, fluid-structure-thermal interactions (where aerodynamic loads, structural response, and heating affect each other), non-equilibrium chemistry (important at high temperatures where air can dissociate and ionize), material ablation (heat shield or surface recession and its effects), and combustion (relevant to air-breathing hypersonic propulsion). Projects that connect these physics to better predictive simulation tools and workflows align with the call’s intent.
HVSI’s stated objectives provide a good sense of what a strong research concept would aim to deliver. Beyond generating new science, the program wants to (1) help develop and document a national vision for hypersonic vehicle simulation, (2) co-fund work that fills gaps not currently covered by DoD, DOE, NASA, or industry efforts but is still critical to DoD hypersonic simulation goals, (3) transition research results into production-quality simulation software that can be broadly used by government, academia, and industry acquisition partners, (4) establish or contribute to a national repository of verification and validation (V&V) data for hypersonic simulations, and (5) provide computational resources that enable a measurable leap forward in simulation capability. That emphasis on transition, V&V, and measurable capability improvements indicates the program is not only looking for theory, but also for work that can be tested, validated, shared, and integrated into usable tools.
Administratively, the opportunity is categorized as discretionary funding under Science and Technology and other R&D (CFDA 12.800) and is open to essentially any applicant type, subject to any additional eligibility clarifications in the full announcement. The posting lists an award ceiling of $2.4 million, with an expectation of about five awards. White papers were due by 4:30 PM Mountain Time on October 15, 2018, reflecting an initial down-select approach where concise white papers are evaluated first, and full proposals may follow by invitation. Overall, this call is best read as an applied computational hypersonics program: it wants advances in turbulence and related high-speed flow physics, but it especially values work that improves predictive simulation credibility, leverages high-performance computing, and transitions into shared, production-ready tools and datasets for the broader defense hypersonics community.Apply for USAFA BAA 2015 CALL 0005
- The Department of Defense, Air Force Academy in the science and technology and other research and development sector is offering a public funding opportunity titled "Hypersonic Turbulence Models Research" and is now available to receive applicants.
- Interested and eligible applicants and submit their applications by referencing the CFDA number(s): 12.800.
- This funding opportunity was created on Sep 13, 2018.
- Applicants must submit their applications by Oct 15, 2018 White papers due by 1630 Mountain time. (Agency may still review applications by suitable applicants for the remaining/unused allocated funding in 2026.)
- Each selected applicant is eligible to receive up to $2,400,000.00 in funding.
- The number of recipients for this funding is limited to 5 candidate(s).
- Eligible applicants include: Unrestricted (i.e., open to any type of entity above), subject to any clarification in text field entitled Additional Information on Eligibility.
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Frequently Asked Questions (FAQs)
What is the Hypersonic Turbulence Models Research opportunity (USAFA BAA 2015 CALL 0005)?
This is a U.S. Department of Defense research opportunity run through the U.S. Air Force Academy (USAFA). It solicits unclassified research white papers first, and then (if the government requests) invites selected teams to submit full proposals later.
Is this a request for white papers or full proposals?
The initial submission is a white paper. The government may invite full proposals after evaluating the white papers, meaning it uses a down-select process rather than requesting full proposals from everyone upfront.
Are submissions required to be unclassified?
Yes. The opportunity is explicitly positioned as soliciting unclassified research white papers.
Should applicants include proprietary information in the white paper?
Submissions are expected to avoid proprietary content. If proprietary material is included, the submitter is responsible for clearly marking those sections according to the instructions in USAFA-BAA-2015 Amendment 0003.
What happens if proprietary content is included?
The burden is on the applicant to clearly mark any proprietary sections in accordance with the instructions in USAFA-BAA-2015 Amendment 0003. The call signals that the default expectation is to avoid proprietary content wherever possible.
What types of funding instruments might be used for awards?
The government indicates openness to multiple instrument types, including a grant, cooperative agreement, or contract, depending on the project and subsequent negotiations.
What program is this call associated with?
The call sits under the Hypersonic Vehicle Simulation Institute (HVSI), which supports the DoD High Performance Computing Modernization Program (HPCMP).
What is the main goal of the effort?
The central goal is to significantly improve the realism, reliability, and usefulness of computational simulations for hypersonic vehicles, with an emphasis on advancing simulation capability in ways that can be used in research, design, and acquisition.
How does high-performance computing (HPC) factor into the opportunity?
The opportunity is tied to HPCMP, which focuses on accelerating progress in high-performance computing software and hardware so the DoD can model hypersonic systems more effectively. Proposed work is expected to align with advancing computational simulation capability and leveraging HPC where it enables measurable improvements.
Is the scope limited only to turbulence modeling?
No. While the title emphasizes turbulence models, the scope described is broader and includes coupled, high-fidelity modeling of multiple hypersonic phenomena that impact predictive simulation.
What technical areas are highlighted as being of interest?
The opportunity highlights work improving computational simulation approaches for hypersonic flight, including advances in numerical methods, physics and engineering models, and end-to-end simulation approaches capturing key aerothermodynamic and propulsion phenomena. Specific examples mentioned include turbulence, boundary layer transition, fluid-structure-thermal interactions, non-equilibrium chemistry, material ablation, and combustion.
Does the call support coupled or multi-physics simulation efforts?
Yes. The description emphasizes coupled, high-fidelity modeling across the hypersonic environment, including interactions such as fluid-structure-thermal coupling where aerodynamic loads, structural response, and heating affect one another.
Why are non-equilibrium chemistry and ablation mentioned?
They are called out as important high-temperature hypersonic effects: non-equilibrium chemistry matters when air can dissociate and ionize, and ablation matters when thermal protection materials recede or change and affect the flow and heating environment. The call indicates interest in simulation approaches that capture these effects to improve predictive capability.
Is hypersonic combustion within scope?
Yes. Combustion is mentioned as relevant to air-breathing hypersonic propulsion, and it appears within the listed technical areas of interest.
What kinds of outcomes does HVSI want beyond publishing research results?
HVSI objectives emphasize transition and practical impact. The opportunity describes goals such as helping develop and document a national vision for hypersonic vehicle simulation, co-funding gap-filling work not covered by other organizations (DoD, DOE, NASA, or industry) but still critical to DoD goals, transitioning research into production-quality simulation software, establishing or contributing to a national repository of verification and validation (V&V) data, and providing computational resources that enable a measurable leap forward in simulation capability.
What does "production-quality simulation software" mean in the context of this call?
Based on the description, it refers to simulation capabilities that move beyond isolated research codes and toward robust, usable tools that government teams and their academic and industry partners can apply broadly.
What is the role of verification and validation (V&V) in this opportunity?
V&V is explicitly emphasized as a program objective. The opportunity notes an interest in establishing or contributing to a national repository of hypersonic simulation V&V data, signaling value for projects that can be tested, validated, and credibly assessed.
Who is eligible to apply?
The posting states the opportunity is open to essentially any applicant type, subject to any additional eligibility clarifications in the full announcement.
How is the opportunity categorized administratively?
It is categorized as discretionary funding under Science and Technology and other R&D, with CFDA 12.800.
What is the maximum award amount (award ceiling)?
The posting lists an award ceiling of $2.4 million.
How many awards are expected?
The opportunity indicates an expectation of about five awards.
When were white papers due?
White papers were due by 4:30 PM Mountain Time on October 15, 2018.
What does the white paper down-select process imply for applicants?
It implies the government intends to evaluate concise concepts first and only invite a subset of applicants to submit full proposals later, focusing proposal effort on the most promising white paper submissions.
What kinds of projects appear to fit best with the call's intent?
Projects that improve predictive hypersonic simulation credibility and usefulness, leverage high-performance computing to achieve measurable advances, and support transition into broadly usable tools and datasets (including V&V data) align closely with the intent described.
Is the opportunity focused on basic theory or applied capability?
The description points strongly toward applied computational hypersonics: it values scientific advances, but it also emphasizes transition, verification/validation, shared repositories, and integration into robust simulation capabilities used by the broader defense hypersonics community.
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