Turbine engines - Study guides, Class notes & Summaries

How are guided missiles classified? According to their range, speed, launch environment, mission, and vehicle type A long-range guided missile can travel what distance? At least 100 miles What missile does not exceed the range capabilities of long-range guns? The short-range guided missile How is the speed capability of guided missiles expressed? In Mach numbers What is a Mach number? The ratio of the speed of an object to the speed of sound in the medium through...

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DDG 1/3 Bell - 0-7 knots DDG 2/3 Bell - 8-12 knots DDG Standard Bell - 13-19 knots DDG Full Bell - 20-27 knots DDG Flank Bell - 28+ knots DDG Max Bell - 30+ knots DDG Displacement - 9200 tons DDG Beam - Hull: 66 ft (SLQ-32 decks overhang 4 feet on each side) DDG Shadow Distance - 160 ft DDG Propulsion Plant - 4 Gas Turbine Engines 100,000 total shaft HP DDG Electrical Plant - 3 Gas Turbine Engines DDG Height of Eye - 56 ft DDG Air Draft - 122 ftDDG Draft - 32.5 ft DDG Length - 509...

Powerplant Turbine Engines Questions With Complete Solutions

Powerplant: Turbine Engines Questions With Complete Solutions

2 - AMT - Powerplant - Turbine Engines (121) Questions With Complete Solutions

Powerplant Orals Exam: Recip Engines, Turbine Engines, Engine Inspections Questions and Answers

Turbine Engines-Power Plant Written Exam Questions Correctly Answered. 1 (8108) - At what point in an axial-flow turbojet engine will the highest gas pressures occur? - CORRECT ANSWER C- At the compressor outlet. 2 (8109) - One function of the nozzle diaphragm in a turbine engine is to - CORRECT ANSWER C- Direct the flow of gases to strike the turbine blades at the desired angle. 3 (8110) - What is the profile of a turbine engine compressor blade? - CORRECT ANSWER B- A reduced blade t...

2 - AMT - Powerplant - Turbine Engines (121) | with complete solution | Latest 2-2024/25

Turbine Engines Study Exam Questions Correctly Answered. 1. What are the two basic sections of a turbine engine? - CORRECT ANSWER The hot section and the cold section. 2. What are the two basic types of compressors that are used in aircraft turbine engines? - CORRECT ANSWER Axial-flow and centrifugal. 3. What is the purpose of the stators in an axial-flow compressor? - CORRECT ANSWER The stators convert some velocity energy into pressure energy and change the direction of the air so i...

Gas Turbine Engines - Performance Question and answers rated A+ 2023/2024Gross thrust - correct answer Forward acting gas load forces - rearward acting gas load forces. Measured at static thrust (no velocity) as a baseline. Thrust specific fuel consumption - correct answer Ratio of the mass of fuel required to produce a unit of power per unit of time. What does thrust specific fuel consumption measure? - correct answer Engine efficiency As Pressure Altitude increases, what will happen t...

1 (8108) - At what point in an axial-flow turbojet engine will the highest gas pressures occur? correct answers C- At the compressor outlet. 2 (8109) - One function of the nozzle diaphragm in a turbine engine is to correct answers C- Direct the flow of gases to strike the turbine blades at the desired angle. 3 (8110) - What is the profile of a turbine engine compressor blade? correct answers B- A reduced blade tip thickness. 4 (8111) - The fan rotational speed of a dual axial compressor...