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Status and outlook of CFD technology at Mitsubishi Heavy Industries Nagoya. Mitsubishi Meiko ni okeru CFD gijutsu no genjo to tenbo

Technical Report:

Abstract

The present and future were reviewed of CFD (computational fluid dynamics) technology in Nagoya Works, Mitsubishi Heavy Industries, Ltd., Japan. The progress of the role of CFD in aerodynamic design and progress of CFD technology were reviewed. The followings were illustrated as examples of CFD analysis: design of a main wing for transonic private aircrafts by backward analysis, analysis of an airframe shape for the MU300 jet airplane with a panel method, Navier-stokes (NS) analysis of a transonic wing section, NS analysis of pressure distributions on the surfaces of the YXX airplane and space shuttle HOPE, and NS analysis of an aerodynamic heating distribution for spaceplanes. CFD tools were outlined for every developmental item such as a main wing, and requirements and subjects in practical use were discussed of several CFD tools for a rough check, precise performance check and parametric study. Such computer performance as a main memory capacity and processing speed required for the future practical use of advanced CFD was also discussed. 20 figs.
Authors:
Tanioka, T [1] 
  1. Mitsubishi Heavy Industries, Ltd., Tokyo (Japan)
Publication Date:
Sep 01, 1990
Product Type:
Technical Report
Report Number:
SP-13
Reference Number:
NEDO-91-930069; EDB-91-130810
Resource Relation:
Related Information: In: Proceedings of the 8th NAL symposium on aircraft computational aerodyanmics, 116 p.
Subject:
97 MATHEMATICS AND COMPUTING; 42 ENGINEERING; 32 ENERGY CONSERVATION, CONSUMPTION, AND UTILIZATION; AERODYNAMICS; AERODYNAMIC HEATING; COMPUTERS; NAVIER-STOKES EQUATIONS; PARAMETRIC ANALYSIS; PRESSURE GRADIENTS; AIRCRAFT; AIRFOILS; SHAPE; TRANSONIC FLOW; TURBOFAN ENGINES; SPACE VEHICLES; DIFFERENTIAL EQUATIONS; ENGINES; EQUATIONS; FLUID FLOW; FLUID MECHANICS; HEATING; MACHINERY; MECHANICS; PARTIAL DIFFERENTIAL EQUATIONS; TURBOMACHINERY; VEHICLES; 990200* - Mathematics & Computers; 420400 - Engineering- Heat Transfer & Fluid Flow; 320201 - Energy Conservation, Consumption, & Utilization- Transportation- Air & Aerospace
OSTI ID:
7843449
Research Organizations:
National Aerospace Lab., Chofu, Tokyo (Japan)
Country of Origin:
Japan
Language:
Japanese
Other Identifying Numbers:
Other: ON: DE91522957
Availability:
OSTI; NTIS (US Sales Only)
Submitting Site:
NEDO
Size:
Pages: 69-81
Announcement Date:
Oct 01, 1991

Technical Report:

Citation Formats

Tanioka, T. Status and outlook of CFD technology at Mitsubishi Heavy Industries Nagoya. Mitsubishi Meiko ni okeru CFD gijutsu no genjo to tenbo. Japan: N. p., 1990. Web.
Tanioka, T. Status and outlook of CFD technology at Mitsubishi Heavy Industries Nagoya. Mitsubishi Meiko ni okeru CFD gijutsu no genjo to tenbo. Japan.
Tanioka, T. 1990. "Status and outlook of CFD technology at Mitsubishi Heavy Industries Nagoya. Mitsubishi Meiko ni okeru CFD gijutsu no genjo to tenbo." Japan.
@misc{etde_7843449,
title = {Status and outlook of CFD technology at Mitsubishi Heavy Industries Nagoya. Mitsubishi Meiko ni okeru CFD gijutsu no genjo to tenbo}
author = {Tanioka, T}
abstractNote = {The present and future were reviewed of CFD (computational fluid dynamics) technology in Nagoya Works, Mitsubishi Heavy Industries, Ltd., Japan. The progress of the role of CFD in aerodynamic design and progress of CFD technology were reviewed. The followings were illustrated as examples of CFD analysis: design of a main wing for transonic private aircrafts by backward analysis, analysis of an airframe shape for the MU300 jet airplane with a panel method, Navier-stokes (NS) analysis of a transonic wing section, NS analysis of pressure distributions on the surfaces of the YXX airplane and space shuttle HOPE, and NS analysis of an aerodynamic heating distribution for spaceplanes. CFD tools were outlined for every developmental item such as a main wing, and requirements and subjects in practical use were discussed of several CFD tools for a rough check, precise performance check and parametric study. Such computer performance as a main memory capacity and processing speed required for the future practical use of advanced CFD was also discussed. 20 figs.}
place = {Japan}
year = {1990}
month = {Sep}
}