Drag Decomposition Using Partial-Pressure Fields: ONERA M6 Wing

Author:

Hart Pierce L.1,Schmitz Sven1

Affiliation:

1. Pennsylvania State University, State College, Pennsylvania 16802

Funder

Aeronautics Research Mission Directorate

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference35 articles.

1. JonesB.LaboratoryC. U. A.BritainA. R. C. G.CommitteeA. M. A. R. “The Measurement of Profile Drag by the Pitot-Traverse Method,” Aeronautical Research Committee Repts. and Memoranda, H.M. Stationery Office 1688, London, 1936.

2. MaskellE. C. “Progress Towards a Method for the Measurement of the Components of the Drag of a Wing of Finite Span,” Royal Aircraft Establishment, Procurement Executive, Ministry of Defence TR 72232, 1972.

3. Shock Waves and Drag in the Numerical Calculation of Compressible, Irrotational Transonic Flow

4. LockR. “Prediction of the Drag of Wings at Subsonic Speeds by Viscous/Inviscid Interaction Techniques,” Advisory Group for Aerospace Research and Development AR 138, 1985.

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