Influence of the inlet Mach number and size of its throat on the symmetrical nozzle flow by small disturbance equation method-Reference-Cited by-同舟云学术

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Influence of the inlet Mach number and size of its throat on the symmetrical nozzle flow by small disturbance equation method

Published:2022-05-17 Issue: Volume: Page:
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Container-title:2nd International Conference on Applied Mathematics, Modelling, and Intelligent Computing (CAMMIC 2022)
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Author:

Fang Ruiyuan

Publisher

SPIE

Reference6 articles.

1. Exhaust Nozzle Contour for Optimum Thrust

2. Compound-Compressible Nozzle Flow

3. Efficient algorithm for solution of the unsteady transonic small-disturbance equation

4. Free boundary problems for the unsteady transonic small disturbance equation: Transonic regular reflection

5. Accurate solutions, parameter studies, and comparisons for the Euler and potential flow equations;Anderson,1988

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