Monotone nozzle shape by direct method

Yuri S. Volkov, Vladislav M. Galkin

Результат исследования: Материалы для книги/типы отчетовГлава


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
Заголовок главной публикацииNew Developments in Mathematics Research
ИздательNova Science Publishers, Inc.
Количество страниц41
ISBN (печатная версия)9781613242520
Статус публикацииОпубликовано - 2011


ASJC Scopus subject areas

  • Mathematics(all)


Volkov, Y. S., & Galkin, V. M. (2011). Monotone nozzle shape by direct method. В New Developments in Mathematics Research (стр. 43-83). Nova Science Publishers, Inc..