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RESEARCH IN FLIGHT LLC
UEI: NN8QT8JVKRH5
# of Employees: 3
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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A Multi-Fidelity Supersonic Flow Solver for Preliminary Design & Optimization
Amount: $50,000.00Research in Flight (RIF) and Utah State University (USU) are proposing the development of a novel supersonic panel method solver which runs on an unstructured mesh and uses low-order surface-vorticity ...
STTRPhase I2022Department of Defense Air Force -
Air Vehicle Gust Response Analysis for Conceptual Design
Amount: $749,999.00The Controls and Load Alleviation Simulation Platform (CLASP) framework was developed in the NASA STTR Phase I activity preceding this Phase II proposal. CLASP has been created to perform time-domain ...
STTRPhase II2021National Aeronautics and Space Administration -
Electric Scalable Aerial Transport (eSCAT)
Amount: $150,000.00A combined industry-academia team of Research in Flight, Flugauto and Auburn University propose the development of Electric, Scalable, Agile Aerial Transport (e-SCAT) specifically designed to meet the ...
STTRPhase I2021Department of Defense Air Force -
Improvement of Multi-Rotor Aerial Vehicles Performance Using Reduced-Order Aero-Mechanical Models
Amount: $150,000.00Research in Flight and Auburn University are teaming to offer a tool capable of providing dramatically improved aeromechnaical mechanisms for the eVTOL/UAM industry. These vehicles must be configure ...
STTRPhase I2021Department of Defense Air Force -
Electric Extended Range Airship with Modular Payload (e2-RAMP)
Amount: $150,000.00A combined industry-academia team of Research in Flight, Skyborne Technology and Auburn University propose the development of Electric Extended Range Airship with Modular Payload (e2-RAMP) specificall ...
STTRPhase I2021Department of Defense Air Force -
Early-Design Aeroacoustics Prediction for Distributed Electric Propulsion Vehicles using FlightStream
Amount: $124,988.00Research in Flight and Auburn University are proposing to develop a robust tool and methodology to allow the simulation and modeling of acoustic signatures for Distributed Electric Propulsion (DEP) ai ...
STTRPhase I2020National Aeronautics and Space Administration -
Air Vehicle Gust Response analysis for Conceptual Design
Amount: $124,998.00Research in Flight (RIF) and Auburn University are offering the development of an advanced, robust tool and methodology that allows the simulation and modeling of gust and wake vortex encounters for D ...
STTRPhase I2019National Aeronautics and Space Administration -
Robust Prediction of High Lift Using Surface Vorticity
Amount: $750,000.00FlightStream has been developed a fast, accurate, aerodynamic prediction code based on vorticity computations on the surface of an aircraft. The code, though still a surface paneling algorithm, has pr ...
SBIRPhase II2017National Aeronautics and Space Administration -
Robust Prediction of High Lift Using Surface Vorticity
Amount: $125,000.00Research in Flight is proposing to advance the capabilities of its surface vorticity solver for aerodynamic loads on subsonic aircraft to include more robust solutions for high lift configurations. A ...
SBIRPhase I2016National Aeronautics and Space Administration -
Advanced Aerodynamic Analysis For Propulsion Airframe Integration
Amount: $123,473.00Research in Flight is proposing to develop a fundamentally new, lower order, high fidelity solution approach for the aerodynamic analysis required for engine integration studies. This new approach is ...
SBIRPhase I2015National Aeronautics and Space Administration
