Improvement of Drag Prediction for Transonic Transport Aircraft Configuration Using Hybrid Unstructured Navier-Stokes Solver.
Author:
Affiliation:
1. 3rd Research Center, TRDI, Japan Defense Agency
2. Mitsubishi Heavy Industries, Ltd.
Publisher
Japan Society of Mechanical Engineers
Subject
Fluid Flow and Transfer Processes,Physical and Theoretical Chemistry,Mechanical Engineering
Link
http://www.jstage.jst.go.jp/article/jsmeb/45/4/45_4_820/_pdf
Reference20 articles.
1. Re-Engineering the Design Process Through Computation
2. (2) Oki, Y., Sakata, T., Uchiyama, N., Kaiden, T. and Ando, T., Numerical Simulation of Transonic Flow past an F-16A Aircraft Configuration Using CASPER, AIAA Paper 2000-0125, (2000).
3. (3) Spalart, P. R. and Allmaras, S. R., A One-Equation Turbulence Model for Aerodynamic Flows, AIAA Paper 92-0439, (1992).
4. (5) Staff of the Second Aerodynamics Division, Results of the Test on ONERA Calibration Model M5 in NAL 2m×2m Transonic Wind Tunnel, NAL TR-774T, (1983).
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