DGCA & EASA Module 15 : Part-1 Gas Turbine Engine Fundamentals Exam with suitable question and verified answers

CA & EASA Module 15 : Part-1 Gas Turbine Engine Fundamentals Exam with suitable question and verified answers 1. A: On an axial flow, dual compressor forward fan engine, the fan turns the same speed as the. A. low pressure turbine. B. high pressure compressor. C. forward turbine wheel. 2. A: A turbo jet engine gives. A. large acceleration to a small mass of air. B. large acceleration to a large weight of air. C. small acceleration to a large mass of air. 3. C: The basic gas turbine engine is divided into two main sections: the cold section and the hot section. A. The cold section includes the engine inlet, compressor, and turbine sections. B. The hot section includes the combustor, diffuser, and exhaust. C. The hot section includes the combustor, turbine, and exhaust. 4. C: A jet engine derives its thrust by. A. drawing air into the compressor. B. impingement of the propelling gases on the outside air. C. reaction of the propelling gases. 5. A: Which of the following might be used to identify turbine discharge pressure?.