Calculation of nozzle flows using Pade fractions.

Author:

VAN TUYL ANDREW H.1

Affiliation:

1. U.S. Naval Ordnance Laboratory, Silver Spring, Md.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 10 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. COMPUTER-EXTENDED SERIES;ANNU REV FLUID MECH;1984

2. Direct method for calculating the transonic flow field in nozzles;16th Aerospace Sciences Meeting;1978-01-16

3. Convergence Acceleration of Relaxation Solutions for Transonic Flow Computations Mohamed;AIAA Journal;1977-03

4. The use of Pade fractions in the calculation of nozzle flows;Padé Approximants Method and Its Applications to Mechanics;1976

5. Application of methods for acceleration of convergence to the calculation of singularities of transonic flows;Padé Approximants Method and Its Applications to Mechanics;1976

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