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Second symposium on numerical and physical aspects of aerodynamic flows California State University, Long Beach, U.S.A. 17–20 January 1983
Computers and FlJdds Vol. I0,No. 4, pp. 307-309,19$2. Pergamon Press Ltd. Priatedin Great Britain.
ANNOUNCEMENTS SECOND SYMPOSIUM ON NUMERICAL AND PHYSICAL ASPECTS OF AERODYNAMIC FLOWS California State University, Long Beach, U.S.A. 17-20 January 1983
This International Symposium will assemble leading research workers, together with users and potential users of their work, to present, consider and discuss numerical and physical aspects of aerodynamic flows. Emphasis will be directed towards flows of relevance to lifting bodies and particularly to their calculation. The two main purposes of the Symposium are: 1. The presentation of technical papers which will provide a basis for research workers to evaluate the present state of the art and formulate priorities for the future. 2. Schedules and informal discussions to assist the improvement of understanding and communication and the development of novel concepts. The program includes: Two Keynote Lectures: Problems Associated With the Design of Missile Shapes, by J. Nielsen. Problems Associated With the Design of Wings, by A. M. O. Smith. Approximately 40 technical papers in Sessions entitled: Numerical Methods for Interactive Flows Measurements and Calculations of Two-Dimensional Interactive Flows Measurements and Calculations of Three-Dimensional Flows: Subsonic Wings Measurements and Calculations of Three-Dimensional Flows: Transonic Wings Measurements and Calculations of Three-Dimensional Flows: Ships and Missiles Two Open-Forum Sessions to allow the reporting and discussion of very recent work on: Separated and Near- Wake Flows--Chairman: K. Stewartson. Flow Around Wings, Ships and Missiles--ChaJrman: D. Bushnell. A Panel Session to consider the question, "What should be the priorities for future research on calculation methods for lifting bodies?"--Chairman: J. H. Whitelaw. A volume of proceedings will be available for participants at the beginning of the Symposium. Further information can be obtained from Tuncer Cebeci, Chief Technology Engineer, Research Aerodynamics Subdivision, Douglas Aircraft Company, 3855 Lakewood Boulevard, Long Beach, CA 90846, U.S.A.
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ANNOUNCEMENTS SECOND SYMPOSIUM ON NUMERICAL AND PHYSICAL ASPECTS OF AERODYNAMIC FLOWS California State University, Long Beach, U.S.A. 17-20 January 1983
This International Symposium will assemble leading research workers, together with users and potential users of their work, to present, consider and discuss numerical and physical aspects of aerodynamic flows. Emphasis will be directed towards flows of relevance to lifting bodies and particularly to their calculation. The two main purposes of the Symposium are: 1. The presentation of technical papers which will provide a basis for research workers to evaluate the present state of the art and formulate priorities for the future. 2. Schedules and informal discussions to assist the improvement of understanding and communication and the development of novel concepts. The program includes: Two Keynote Lectures: Problems Associated With the Design of Missile Shapes, by J. Nielsen. Problems Associated With the Design of Wings, by A. M. O. Smith. Approximately 40 technical papers in Sessions entitled: Numerical Methods for Interactive Flows Measurements and Calculations of Two-Dimensional Interactive Flows Measurements and Calculations of Three-Dimensional Flows: Subsonic Wings Measurements and Calculations of Three-Dimensional Flows: Transonic Wings Measurements and Calculations of Three-Dimensional Flows: Ships and Missiles Two Open-Forum Sessions to allow the reporting and discussion of very recent work on: Separated and Near- Wake Flows--Chairman: K. Stewartson. Flow Around Wings, Ships and Missiles--ChaJrman: D. Bushnell. A Panel Session to consider the question, "What should be the priorities for future research on calculation methods for lifting bodies?"--Chairman: J. H. Whitelaw. A volume of proceedings will be available for participants at the beginning of the Symposium. Further information can be obtained from Tuncer Cebeci, Chief Technology Engineer, Research Aerodynamics Subdivision, Douglas Aircraft Company, 3855 Lakewood Boulevard, Long Beach, CA 90846, U.S.A.
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