Numerical computation of transonic flow about wing-fuselage configurations on a vector computer
Author:
Affiliation:
1. Informatics General Corp., Palo Alto, CA
2. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-499
Reference28 articles.
1. Preliminary study of the use of the STAR-100 computer for transonic flow calculations
2. New Approach to the 3-D Transonic Flow Analysis Using the STAR-106 Computer
3. Vector Processor Algorithms for Transonic Flow Calculations
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1. Approximate factorization scheme for transonic potential flow computations;Sadhana;1992-06
2. Transonic Euler solutions on a blunt, body-wing-canard configuration;Journal of Spacecraft and Rockets;1988-11
3. A comparison of explicit and implicit three-dimensional split flux Euler algorithms;5th Applied Aerodynamics Conference;1987-08-17
4. Transonic flow solutions on a blunt, body-wing-canard configuration using the Euler equations;5th Applied Aerodynamics Conference;1987-08-17
5. Simulation of external flowfields using a three-dimensional Euler/Navier-Stokes algorithm;25th AIAA Aerospace Sciences Meeting;1987-03-24
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