Questions › Category: Compressors Gas Turbines and Jet EnginesFilter:AllOpenResolvedClosedUnansweredSort byViewsAnswersVotesThe absolute pressure of air at the outlet of a compressor is calledOpenVideRime asked 2 years ago • Compressors Gas Turbines and Jet Engines113 views0 answers0 votesFor supplying intermittent small quantity of air at high pressure, following compressor is best suitedOpenVideRime asked 2 years ago • Compressors Gas Turbines and Jet Engines100 views0 answers0 votesIn n₁ and n₂ are the indices of compression for the first and second stage of compression, then the ratio of work-done on the first and second stages (W₁/W₂) with perfect intercooling is given byOpenVideRime asked 2 years ago • Compressors Gas Turbines and Jet Engines273 views0 answers0 votesWhich of the following statement is correct? (A) The ratio of the discharge pressure to the inlet pressure of air is called compressor efficiency (B) The compression ratio for the compressor is always greater than unity OpenVideRime asked 2 years ago • Compressors Gas Turbines and Jet Engines138 views0 answers0 votesThe indicated work per unit mass of air delivered isOpenVideRime asked 2 years ago • Compressors Gas Turbines and Jet Engines115 views0 answers0 votesIf p₁, is the pressure of air entering the L.P. cylinder and p₂ is the pressure of air leaving the L.P. cylinder (or inter-cooler pressure), then the ratio of cylinder diameters for a single acting, two stage reciprocating air compressor with complete intercooling is given by (where D₁ = Dia. of L.P. cylinder, and D₂ = Dia. of H.P. cylinder)OpenVideRime asked 2 years ago • Compressors Gas Turbines and Jet Engines279 views0 answers0 votesThe volumetric efficiency of a compressor falls roughly as follows for every 5°C increase in atmospheric temperatureOpenVideRime asked 2 years ago • Compressors Gas Turbines and Jet Engines104 views0 answers0 votesThe axial flow compressor is preferred in aircraft gas turbines because ofOpenVideRime asked 2 years ago • Compressors Gas Turbines and Jet Engines119 views0 answers0 votesLosses in a centrifugal compressor are due toOpenVideRime asked 2 years ago • Compressors Gas Turbines and Jet Engines126 views0 answers0 votesWhen the temperature of air leaving the inter-cooler, in a two stage compression with inter-cooler, is ________ the original atmospheric air temperature, then the intercooling is known as perfect or complete intercooling.OpenVideRime asked 2 years ago • Compressors Gas Turbines and Jet Engines130 views0 answers0 votes