ONE OF THE GOALS OF NASA'S FUNDAMENTAL AERONAUTICS "SUBSONIC FIXED WING" PROJECT IS TO REDUCE FUEL BURN BY…
Award details are derived from public USAspending.gov records. Not a bid recommendation.
Award details
- Award ID
- NNX10CE81P
- Contractor
- Awarding agency
- National Aeronautics and Space Administration
- Sub-agency / office
- National Aeronautics and Space Administration
- Award amount
- $0
- Period of performance
- Jan 29, 2010 – Jul 29, 2010
- NAICS
- 541712 — Research and Development in the Physical, Engineering, and Life Sciences
- PSC
- PSC AR11
- Place of performance
- CA
Public award description
ONE OF THE GOALS OF NASA'S FUNDAMENTAL AERONAUTICS "SUBSONIC FIXED WING" PROJECT IS TO REDUCE FUEL BURN BY 25% 5% BY 2018. THIS CORRESPONDS APPROXIMATELY TO AN INCREASE IN LIFT/DRAG RATIO OF THE SAME MAGNITUDE. WHILE THE IMPROVEMENT IN DESIGN TOOLS FUNDED BY NASA WILL UNDOUBTEDLY HELP ATTAIN THIS GOAL THE INNOVATION PROPOSED HERE IS AN ADDITION TO THIS EFFORT. IN OTHER WORDS, ANY IMPROVEMENTS IN PERFORMANCE DUE TO THE INNOVATION SHOULD BE ADDED TO ANY IMPROVEMENTS DUE TO THE USE OF NEW DESIGN TOOLS. THE INNOVATION PROPOSED HERE IS A "LEADING EDGE WAVE" IN WHICH THE LEADING EDGE OF A WING IS DESCRIBED BY A HIGH FREQUENCY, LOW AMPLITUDE WAVE, RATHER THAN THE MORE CONVENTIONAL STRAIGHT LINE. PREVIOUS RESULTS HAVE INDICATED THAT SUCH A LEADING EDGE CAN LEAD TO IMPROVEMENTS IN LIFT/DRAG RATIO OF 15%.
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