Theoretical Modelling of Aeroheating on Sharpened Noses Under Rarefied Gas Effects and Nonequilibrium Real Gas Effects (Record no. 52036)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 03126nam a22005295i 4500 |
| 001 - CONTROL NUMBER | |
| control field | 978-3-662-44365-1 |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20200420220223.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 140828s2015 gw | s |||| 0|eng d |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| ISBN | 9783662443651 |
| -- | 978-3-662-44365-1 |
| 082 04 - CLASSIFICATION NUMBER | |
| Call Number | 620.1064 |
| 100 1# - AUTHOR NAME | |
| Author | Wang, Zhi-Hui. |
| 245 10 - TITLE STATEMENT | |
| Title | Theoretical Modelling of Aeroheating on Sharpened Noses Under Rarefied Gas Effects and Nonequilibrium Real Gas Effects |
| 300 ## - PHYSICAL DESCRIPTION | |
| Number of Pages | XV, 94 p. 46 illus., 27 illus. in color. |
| 490 1# - SERIES STATEMENT | |
| Series statement | Springer Theses, Recognizing Outstanding Ph.D. Research, |
| 505 0# - FORMATTED CONTENTS NOTE | |
| Remark 2 | Introduction -- Theoretical Modeling of Aeroheating under Rarefied Gas Effects -- Theoretical modeling of the chemical nonequilibrium flow behind a normal shock wave -- Theoretical modeling of aero-heating under nonequilibrium real gas effects -- Conclusions and prospect. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc | Theoretical Modelling of Aeroheating on Sharpened Noses under Rarefied Gas Effects and Nonequilibrium Real Gas Effects employs a theoretical modeling method to study hypersonic flows and aeroheating on sharpened noses under rarefied gas effects and nonequilibrium real gas effects that are beyond the scope of traditional fluid mechanics. It reveals the nonlinear and nonequilibrium features, discusses the corresponding flow and heat transfer mechanisms, and ultimately establishes an analytical engineering theory framework for hypersonic rarefied and chemical nonequilibrium flows. The original analytical findings presented are not only of great academic significance, but also hold considerable potential for applications in engineering practice. The study explores a viable new approach, beyond the heavily relied-upon numerical methods and empirical formulas, to the present research field, which could be regarded as a successful implementation of the idea and methodology of the engineering sciences. |
| 856 40 - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | http://dx.doi.org/10.1007/978-3-662-44365-1 |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Koha item type | eBooks |
| 264 #1 - | |
| -- | Berlin, Heidelberg : |
| -- | Springer Berlin Heidelberg : |
| -- | Imprint: Springer, |
| -- | 2015. |
| 336 ## - | |
| -- | text |
| -- | txt |
| -- | rdacontent |
| 337 ## - | |
| -- | computer |
| -- | c |
| -- | rdamedia |
| 338 ## - | |
| -- | online resource |
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| -- | rdacarrier |
| 347 ## - | |
| -- | text file |
| -- | |
| -- | rda |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Engineering. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Fluids. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Fluid mechanics. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Aerospace engineering. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Astronautics. |
| 650 14 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Engineering. |
| 650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Engineering Fluid Dynamics. |
| 650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Fluid- and Aerodynamics. |
| 650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Aerospace Technology and Astronautics. |
| 830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE | |
| -- | 2190-5053 |
| 912 ## - | |
| -- | ZDB-2-ENG |
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