Application of Drag Reduction Techniques to Transport Aircraft

Author:

Malik Mujeeb R.1,Crouch Jeffrey D.2,Saric William S.3,Lin John C.1,Whalen Edward A.4

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

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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