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Modern aerodynamic methods for direct and inverse applications / by Wilson C. Chin.

By: Material type: TextTextLanguage: English Publication details: Beverly, M.A : Scrivener Publishing, 2019.Description: xiv, 426 p. : ill. ; 24 cmISBN:
  • 9781119580560
Subject(s): DDC classification:
  • 629.1323 CHI/M
Summary: This book helps readers approach the literature more critically. Rather than simply understanding an approach, for instance, the powerful "type differencing" behind transonic analysis, or the rationale behind "conservative" formulations, or the use of Euler equation methods for shear flow analysis when they are unnecessary, the author guides and motivates the user to ask why and why not and what if. And often, more powerful methods can be developed using no more than simple mathematical manipulations. For example, Cauchy-Riemann conditions, which are powerful tools in subsonic airfoil theory, can be readily extended to handle compressible flows with shocks, rotational flows, and even three-dimensional wing flowfields, in a variety of applications, to produce powerful formulations that address very difficult problems. This breakthrough volume is certainly a "must have" on every engineer's bookshelf.
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Holdings
Item type Current library Home library Collection Call number Status Date due Barcode Item holds
Technical Reference Book Technical Reference Book Central Library, IIT Bhubaneswar Central Library, IIT Bhubaneswar SMS 629.1323 CHI/M (Browse shelf(Opens below)) Available 10876
Total holds: 0

Includes bibliographical references and index.

This book helps readers approach the literature more critically. Rather than simply understanding an approach, for instance, the powerful "type differencing" behind transonic analysis, or the rationale behind "conservative" formulations, or the use of Euler equation methods for shear flow analysis when they are unnecessary, the author guides and motivates the user to ask why and why not and what if. And often, more powerful methods can be developed using no more than simple mathematical manipulations. For example, Cauchy-Riemann conditions, which are powerful tools in subsonic airfoil theory, can be readily extended to handle compressible flows with shocks, rotational flows, and even three-dimensional wing flowfields, in a variety of applications, to produce powerful formulations that address very difficult problems. This breakthrough volume is certainly a "must have" on every engineer's bookshelf.

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