Calculation of nozzle flows using Pade fractions.
Author:
Affiliation:
1. U.S. Naval Ordnance Laboratory, Silver Spring, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6782
Reference12 articles.
1. Modern advances in the physics of gasdynamic lasers
2. A Summary of Recent Research on Continuous-Wave Chemical Lasers
3. Effect of small radius of curvature on transonic flow in axisymmetric nozzles.
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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