SBIR/STTR Research Award

Advanced Chemically-Based Actuation for Active Flow Control

Award identifier 13e75b357445077361be903416ed7f6a9209953199195cc7b4d312fd50d96a83Awarding agency National Aeronautics and Space Administration

Award amount

$123,796

Program and phase

SBIR · Phase I

Award year

2017

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Virtual Aerosurface Technologies, Inc.
Proposal award date
2017-06-09
Contract end date
2017-12-08
UEI
ZC8YQ5K8MB83
Solicitation number
Not reported
Topic code
A1.04

Research abstract

The proposed SBIR program by Virtual AeroSurface Technologies (VAST) focuses on the development of a novel variant of pulsed blowing active flow control in which chemically-based flow control actuators are utilized to create high-impulse pulsed jets from discrete reaction chambers with a flowable propellant mixture provided to each. Chemically-based actuation is capable of producing high-impulse jets with sufficient control authority for full-scale flight vehicles and speeds, and, compared to other pulsed blowing flow control schemes, this type of actuation inherently requires less energy from other flight systems as the energy used to create the high jet momentum is stored chemically within the propellant. This general actuation approach has been successfully demonstrated before in the form of COMPACT (in which gaseous fuel and air are repetitively combusted to form pulsed jets for control of separation) and gas generator actuators (in which microfabricated combustion chambers with solid propellant mixtures are utilized for single-shot trajectory control of spin-stabilized projectiles). The innovation proposed here (in which flowable propellant is dynamically supplied to the chambers from an integrated local reservoir) will eliminate the challenges and infrastructure associated with supplying large volumes of air which are necessary for most pulsed blowing approaches and, to a lesser extent, for COMPACT. The proposed Phase I program will investigate multiple propellant chemical compositions, mechanisms for delivering the fuel and oxidizer compounds to the actuator chamber, and methodology for successful repetitive initiation of the chemical reaction within the chamber. A benchtop prototype with repetitive firing will be demonstrated at the end of the Phase I program. A prospective Phase II follow-on program will proceed to develop and demonstrate large arrays of these actuators and perform wind tunnel demonstrations of their utility for active flow control.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

9 SBIR/STTR records share this UEI (2004–2017). Reported award amounts total $3,168,349. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration

Agency intelligence

National Aeronautics and Space Administration

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