Application of Drag Reduction Techniques to Transport Aircraft
Author:
Affiliation:
1. NASA Langley Research Center; Hampton VA USA
2. Boeing Commercial Airplanes; Seattle WA USA
3. Department of Aerospace Engineering; Texas A&M University; College Station TX USA
4. Boeing Research & Technology; Hazelwood MO USA
Publisher
John Wiley & Sons, Ltd
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1002/9780470686652.eae1013/fullpdf
Reference31 articles.
1. Arnal , D. Archambaud , J.P. 2008 VKI Lecture Series: Advances in Laminar-Turbulent Transition Modeling
2. Arnal , D. Perraud , J. Séraudie , A. 2008 VKI Lecture Series: Advances in Laminar-Turbulent Transition Modeling
3. Balakumar , P. King , R. Eppink , J. 2014 Effects of forward and backward facing steps on the crossflow receptivity and stability in supersonic boundary layers
4. Bezos-O'Conner , G.M. Mangelsdorf , M.F. Maliska , H.A. Washburn , A.E. Wahls , R.A. 2011 Fuel efficiencies through airframe improvements
5. Bushnell , D.M. 1992 Overview of aircraft drag reduction technology
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