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Separated and Vortical Flow in Aircraft Wing Aerodynamics: Basic Principles and Unit Problems

Separated and Vortical Flow in Aircraft Wing Aerodynamics: Basic Principles and Unit Problems

Hardcover

Technology & EngineeringPhysics

ISBN10: 3662613263
ISBN13: 9783662613269
Publisher: Springer
Published: Oct 5 2020
Pages: 456
Weight: 1.84
Height: 1.06 Width: 6.14 Depth: 9.21
Language: English

Fluid mechanical aspects of separated and vortical flow in aircraft wing aerodynamics are treated. The focus is on two wing classes: (1) large aspect-ratio wings and (2) small aspect-ratio delta-type wings. Aerodynamic design issues in general are not dealt with.

Discrete numerical simulation methods play a progressively larger role in aircraft design and development. Accordingly, in the introduction to the book the different mathematical models are considered, which underlie the aerodynamic computation methods (panel methods, RANS and scale-resolving methods). Special methods are the Euler methods, which as rather inexpensive methods embrace compressibility effects and also permit to describe lifting-wing flow.

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