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Nasa Technical Reports Server (ntrs) 19910007799%3a The Aerospace Plane Design Challenge%3a Credible Computational Fluid Dynamics Results by Nasa Technical Reports Server (ntrs)
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1NASA Technical Reports Server (NTRS) 19910007799: The Aerospace Plane Design Challenge: Credible Computational Fluid Dynamics Results
By NASA Technical Reports Server (NTRS)
Computational fluid dynamics (CFD) is necessary in the design processes of all current aerospace plane programs. Single-stage-to-orbit (STTO) aerospace planes with air-breathing supersonic combustion are going to be largely designed by means of CFD. The challenge of the aerospace plane design is to provide credible CFD results to work from, to assess the risk associated with the use of those results, and to certify CFD codes that produce credible results. To establish the credibility of CFD results used in design, the following topics are discussed: CFD validation vis-a-vis measurable fluid dynamics (MFD) validation; responsibility for credibility; credibility requirement; and a guide for establishing credibility. Quantification of CFD uncertainties helps to assess success risk and safety risks, and the development of CFD as a design tool requires code certification. This challenge is managed by designing the designers to use CFD effectively, by ensuring quality control, and by balancing the design process. For designing the designers, the following topics are discussed: how CFD design technology is developed; the reasons Japanese companies, by and large, produce goods of higher quality than the U.S. counterparts; teamwork as a new way of doing business; and how ideas, quality, and teaming can be brought together. Quality control for reducing the loss imparted to the society begins with the quality of the CFD results used in the design process, and balancing the design process means using a judicious balance of CFD and MFD.
“NASA Technical Reports Server (NTRS) 19910007799: The Aerospace Plane Design Challenge: Credible Computational Fluid Dynamics Results” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19910007799: The Aerospace Plane Design Challenge: Credible Computational Fluid Dynamics Results
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19910007799: The Aerospace Plane Design Challenge: Credible Computational Fluid Dynamics Results” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - AEROSPACE PLANES - COMPUTATIONAL FLUID DYNAMICS - DESIGN ANALYSIS - NATIONAL AEROSPACE PLANE PROGRAM - SUPERSONIC COMBUSTION - CERTIFICATION - COMMERCE - QUALITY CONTROL - RISK - SAFETY - Mehta, Unmeel B.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19910007799
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 41.01 Mbs, the file-s for this book were downloaded 80 times, the file-s went public at Mon Sep 26 2016.
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Abbyy GZ - Animated GIF - Archive BitTorrent - DjVuTXT - Djvu XML - JPEG Thumb - Metadata - Scandata - Single Page Processed JP2 ZIP - Text PDF -
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