Abstract
Miranda, L. R., Application of Computational Aerodynamics to Airplane Design, Journal of Aircraft, Vol. 21, June 1984, pp. 355-370. Hess, J. L., Calculation of Potential Flow about Arbitrary Lifting Bodies, McDonnell Douglas Rept. MDC J5679, Oct. 1972; (see also Computer Methods in Applied Mathematics and Engineering, Vol. 4, No. 3, Nov. 1974). Hess, J. L. and Friedman, D. M., An Higher Order Panel Method for Three-Dimensional Lifting Potential Flow, NADC-79277-60, Dec. 1981. Hess, J. L. and Friedman, D. M., Analysis of Complex Inlet Configurations Using a Higher-Order Panel Method, AIAA Paper 83-1828, July 1983. Hess, J. L., Improved Solution for Potential Flow About Arbitrary Axisymmetric Bodies by Use of a Higher-Order Surface Source Method, Computer Methods in Applied Mechanics and Engineering, Vol. 5, No. 3, May 1975. Duct Internal Pressure Distribution
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
