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Unified Propulsion Problems Part 5-Thermodynamic Propulsion-Assignment Solution, Exercises of Applied Thermodynamics
This is assignment solution for Thermo Propulsion course. It was submitted to Prof. Yogi Banerjee at Kumaun University. It includes: Unified, Propulsion, Cross-sectional, Area, Stream, Tube, Steady, Flow, Symmetry, Pressure, Forces, Flux, Mass
Typology: Exercises
2011/2012
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UMFIED PRoPVLSIOMN PZ SoanvTIONS, WAIT2 4 ! R ‘ 4, 1 Ao) THE Chas SECTIONAL AREA OF THe STRENUTURE | 7 Is Latoer pr BS THAN AT ©. Since Paw Spa 4/ 1S WNCOMPRESSIBLE R= CONST, Ve ew NN, >Vb S) STEADY Flow, No AGL OF CNY a R~ Ra +Gpds - (gustatds ® 3 NoTe: a) BY SYMMETAN ALESSURE FORCES ON UfPER AND LowER SISAAASURFACES WILL BAUIN CE “. ONLY NEED TO ConsidER PRESSURE Farces GN LEST ANDO RiGdT SURFACES GF CV. b) ouice UPPER AND Lewe SURFACES ARE STREAAKLINES CEvert wrerts, PACALEL To Flaw) THERE & No Fux Achess THEM. NEED GNLY “CodSiDER Flex TERMS ON LeFO ASD RLeuT SURFACES QF Cy. Re + PaS~ PLS = QV spa (-Vacspo)s + 6 Vbcespb (Motos) S MASS Flow THtou6d Sere AT @ = OVO C&R«S ANUST 62. EQUAL ALAS FLow THRav6it SINCE NO OTTER Sunkace AT a §Nbas es FLUXES IN OR ° OUT oF eV. e KPa S = fowe am Gv, whaling fore On blade ts’ —~ “pikecTiow docsity.com