Use of Leading Edge Waves to Increase Lift/Drag Ratio

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$98,868.00
Award Year:
2010
Program:
SBIR
Phase:
Phase I
Contract:
NNX10CE81P
Agency Tracking Number:
094153
Solicitation Year:
2009
Solicitation Topic Code:
A2.05
Solicitation Number:
n/a
Small Business Information
David Nixon
1644 Clay Drive, Los Altos, CA, 94024-6251
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
832880517
Principal Investigator:
David Nixon
Principal Investigator
(650) 964-9956
davidnixon@sbcglobal.net
Business Contact:
David Nixon
President
(650) 964-9956
davidnixon@sbcglobal.net
Research Institution:
n/a
Abstract
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%.

* information listed above is at the time of submission.

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