Air Breathing EnginesI. K. International Pvt Ltd, 2010 - 272 σελίδες Examines the theory of air breathing engines - or more precisely aircraft engines. These engines take air from the atmosphere, accelerate and produce thrust to the aircraft. Gas turbine forms the basic unit and is gas generator. The components of the gas turbines are given in detail. The book will be useful for aeronautical engineering students. |
Περιεχόμενα
Ch01_Bharatipdf | 1 |
Ch02_Bharatipdf | 20 |
Ch03_Bharatipdf | 53 |
Ch04_Bharatipdf | 92 |
Ch05_Bharatipdf | 125 |
Ch06_Bharatipdf | 167 |
Ch07_Bharatipdf | 200 |
Ch08pdf | 223 |
Appendix_Tablepdf | 229 |
Appendixpdf | 244 |
Refrencepdf | 246 |
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Συχνά εμφανιζόμενοι όροι και φράσεις
afterburner airbreathing engines airflow altitude ambient pressure blades Brayton cycle burner by-pass ratio C₁ C₂ Chandrayaan cold nozzle combined cycle combustion chamber combustor compression compressor pressure ratio compressor turbine const density energy enthalpy drop equation exhaust gas exhaust nozzle expansion F-P F-P F-P free power turbine fuel-to-air ratio gas turbine hot gases hot nozzle HRSG Hydrazine inlet temperature intake isentropic efficiency jet velocity kg/s kJ/kg kJ/kg.K Mach number mass flow rate mechanical efficiencies moon outlet pressure P₁ P₂ power plant pressure and temperature pressure loss propeller propulsive efficiency reciprocating engine reheat RFNA rocket schematic diagram shaft shown in Fig single spool Solution specific fuel consumption Specific impulse speed spool engine stage stagnation pressure subsonic supersonic T-S diagram T₁ T₂ thermodynamic thrust produced To₂ TSFC turbofan turbofan engine turbojet turbojet engine turboprop turboprop engine W₁