Optimal nozzle design with monotonicity constraints

Yuri S. Volkov, Vladislav M. Galkin

Результат исследований: Материалы для книги/типы отчетовГлава

1 Цитирования (Scopus)

Аннотация

Two classical gas dynamics axisymmetric problems are considered: the design of a supersonic nozzle with a corner point in the minimum cross section and a uniform exit characteristic and the design of a subsonic nozzle part with a plane sonic line in the minimum cross section. Numerical solving was realized by a direct method by means of minimization of a suitable functional with a minimum corresponding to the optimum nozzle profile. At representation of a nozzle profile were used polynomials, splines and logarithmic functions. In some cases minimization with monotonicity constraits on a nozzle profile is the unique reason of success.

Язык оригиналаАнглийский
Название основной публикацииComputer Design and Computational Defense Systems
ИздательNova Science Publishers, Inc.
Страницы93-125
Число страниц33
ISBN (печатное издание)9781611227567
СостояниеОпубликовано - янв 2011

ASJC Scopus subject areas

  • Computer Science(all)

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  • Цитировать

    Volkov, Y. S., & Galkin, V. M. (2011). Optimal nozzle design with monotonicity constraints. В Computer Design and Computational Defense Systems (стр. 93-125). Nova Science Publishers, Inc..