Reduced Order Nonlinear Dynamic Aeroservoelasticity
Award amount
$124,955Program and phase
SBIR · Phase IAward year
2016Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- M4 ENGINEERING, INC.
- Proposal award date
- 2016-06-10
- Contract end date
- 2016-12-09
- UEI
- DM3EW67JLQM1
- Solicitation number
- Not reported
- Topic code
- A1.01
Research abstract
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.
- Hypersonic Computational Fluid Dynamics Heat Flux Sub-Models
- PyFoil81: Rotorcraft Design Tool Airfoil Table Generator
- High-Fidelity Computational Modeling of Fluid-Thermal-Structural Interactions in Hypersonic Air-Breathing Systems
- UAM Design Space Exploration Framework with Embedded Version Control
- Low Cost Carbon-Carbon Development for Hypersonic Flight Systems
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Dynamic Flight Simulation Utilizing High Fidelity CFD-Based Nonlinear Reduced Order Model
- Physics-Based Models for Aeroservoelasticity Prediction and Control
- Single-Process, Unitized, Composite Fuselage
- Interchain Transesterification as a Solid-State Composite Welding Mechanism
- Manufacturing For Design of Titanium Alloys
Research funding history
83 SBIR/STTR records share this UEI (2004–2026). Reported award amounts total $30,097,301. Reported amounts are not federal obligations.
Phases: Phase I, Phase II, Phase II – Direct to Phase II
Agencies: Department of Defense, National Aeronautics and Space Administration