Partial Pressure Field for Airfoil Wave Drag-Reference-Cited by-同舟云学术

Partial Pressure Field for Airfoil Wave Drag

Published:2022-10 Issue:10 Volume:60 Page:5791-5804
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Hart Pierce L.¹,Schmitz Sven¹

Affiliation:

1. Pennsylvania State University, State College, Pennsylvania 16802

Funder

National Aeronautics and Space Administration

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J061690

Reference45 articles.

1. JonesB.LaboratoryC. U. A.BritainA. R. C. G.CommitteeA. M. A. R. “The Measurement of Profile Drag by the Pitot-Traverse Method,” British Aeronautical Research Committee R&M 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. Wake Integration for Three-Dimensional Flowfield Computations: Theoretical Development

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