000			04288nam a22004573i 4500
001			EBC333158
003			MiAaPQ
005			20181121151049.0
006			m o d |
007			cr cnu||||||||
008			181113s2006 xx o ||||0 eng d
020			_a9788122423228 _q(electronic bk.)
020			_z9788122419139
035			_a(MiAaPQ)EBC333158
035			_a(Au-PeEL)EBL333158
035			_a(CaPaEBR)ebr10323307
035			_a(CaONFJC)MIL122436
035			_a(OCoLC)476137881
040			_aMiAaPQ _beng _erda _epn _cMiAaPQ _dMiAaPQ
050		4	_aQC161.5 -- .Y34 2006eb
082	0		_a621.43 _a621.43/0212
100	1		_aYahya, S.M.
245	1	0	_aGas Tables : _bfor Compressible Flow Calculations.
250			_a5th ed.
264		1	_aDaryaganj : _bNew Age International, _c2006.
264		4	_c©2006.
300			_a1 online resource (159 pages)
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
505	0		_aCover -- Preface to the Fifth Edition -- Preface to the First Edition -- Contents -- Notation -- Introduction -- Table 1. Gas dynamic properties of air at various temperatures -- 1.1 Gas dynamic properties of air -- 1.2 Gas dynamic properties of hydrogen -- 1.3 Gas dynamic properties of carbon dioxide -- 1.4 Gas dynamic properties of superheated steam -- 1.5 Gas dynamic properties of superheated Freon-21 -- Table 2. Properties of Standard Atmosphere -- Table 3. Isentropic Flow of Perfect Gases -- 3.1 γ = 1.3 -- 3.2 γ = 1.4 -- 3.3 γ = 1.67 -- Table 4. Normal Shocks in Perfect Gases -- 4.1. (γ = 1.3) -- 4.2. (γ = 1.4) -- 4.3. (γ = 1.67) -- Table 5. Oblique Shocks in Perfect Gases -- Wave Angles for Given Deflection (γ = 1.4 -- Upstream and Downstream Mach Numbers and Deflection from Normal Shock Relations, (γ = 1.4) -- Table 6. Flow of Perfect Gases with Friction (Fanno Flow) -- 6.1 γ = 1.3 -- 6.2 γ = 1.4 -- 6.3 γ = 1.67 -- Table 7. Isothermal Flow of Perfect Gases with Friction -- 7.1 γ = 1.3 -- 7.2 γ = 1.4 -- Table 8. Flow of Perfect Gases with Heat Transfer (Rayleigh Flow) -- 8.1 γ = 1.3 -- 8.2 γ = 1.4 -- 8.3 γ = 1.67 -- Maximum Heat Transfer in Perfect Gases -- Table 9. Prandtl-Meyer Function with Mach Angles -- α and ω (M) as functions of M -- M and α as functions of ω (M) -- Table 10. Approximate Velocities and Mach Numbers of Air -- 10.1 Air velocities and Mach numbers as functions of dynamic heads in mm W.G. -- 10.2 Air velocities and Mach numbers as functions of dynamic heads in mm Hg. -- 10.3 Mach Numbers as functions of pressure ratios (γ = 1.4) -- Table 11. Manometer Inclinations Required for the Desired Magnification of the Deflection -- Table 12. Static Pressure Drop in Gas Pipe Lines -- Table 13. Isentropic Compressor Power -- Table 14. Pumping Power for Fans and Blowers -- Table 15. S.I, Metric and British Units.
505	8		_a15.1. Principal dimensions and units -- Conversion of Units.
520			_aThe subject of compressible flow or gas dynamics deals with the thermo-fluid dynamic problems of gases and vapours. It is now an important part of the undergraduate and postgraduate curricula. Fundamentals of Compressible Flow covers this subject in fourteen well organised chapters in a lucid style. A large mass of theoretical material and equations has been supported by a number of figures and graphical depictions. Author's sprawling teaching experience in this subject and allied areas is reflected in the clarity, and systematic and logical presentation.
588			_aDescription based on publisher supplied metadata and other sources.
590			_aElectronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2018. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.
650		0	_aAir -- Tables.
650		0	_aThermodynamics -- Tables.
655		4	_aElectronic books.
776	0	8	_iPrint version: _aYahya, S.M. _tGas Tables : for Compressible Flow Calculations _dDaryaganj : New Age International,c2006 _z9788122419139
797	2		_aProQuest (Firm)
856	4	0	_uhttps://ebookcentral.proquest.com/lib/buse-ebooks/detail.action?docID=333158 _zClick to View
999			_c57824 _d57824