Can you please answer question 4 Q3. Perform a design point cycle analysis for a non-afterburning turbojet engine at cruiseflight conditions. Take note of the following performance parameters:Diffuser: nd = 0.97; yd = 1.4;Compressor: nc = 0.95; yc = 1.37; π = 20;Burner: nb = 1; yb = 1.35; πb = 0.95; T_max = 1500Kqr = 45 MJ/kg of fuelTurbine: nt = 0.90; yt = 1.33; nm = 0.99Core nozzle: nn = 0.98; yn = 1.36Current flight conditions at 12200 m cruise altitude, and cruise Mach number of 0.85.Given the above flight and engine information, determine the specific thrust, TSFC, andoverall efficiency.Q4. A twin-engine light cargo aircraft has a take-off weight of 10 000 lb and for a reasonabletake-off distance, requires a F/W at 50 mph of 0.25 at SSL conditions. The propellerdiameter is 7ft. Assuming the required engine shaft power to drive the propeller is 1.22times the ideal actuator disk power, estimate the needed shaft power delivered by eachengine.End of Part B

Answered: Image /qna-images/answer/b363bfcc-077f-4a80-b124-9d57b79248f0.jpg

Q4. A twin-engine light cargo aircraft has a take-off weight of 10 000 lb and for a reasonable take-off distance, requires a F/W at 50 mph of 0.25 at SSL conditions. The propeller diameter is 7ft. Assuming the required engine shaft power to drive the propeller is 1.22 times the ideal actuator disk power, estimate the needed shaft power delivered by each engine.

Q4. A twin-engine light cargo aircraft has a take-off weight of 10 000 lb and for a reasonable take-off distance, requires a F/W at 50 mph of 0.25 at SSL conditions. The propeller diameter is 7ft. Assuming the required engine shaft power to drive the propeller is 1.22 times the ideal actuator disk power, estimate the needed shaft power delivered by each engine.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Essay Topic: Define the following terms related to reciprocating engines: cycle, stroke, bore, clearance volume, volume displacement, clearance percentage, compression ratio, cut-off ratio, pressure ratio, and thermal efficiency.
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