Solution 1 Exercise 7 Climb 1 Given conditions of Saw tooth climb flight test Pressure Altitude 2000 ft Single engine Temperature Standard
Solution Exercise Climb Given conditions of Saw tooth climb flight test Pressure Altitude
Solution Exercise Climb Given conditions of Saw tooth climb flight
Given conditions of Saw tooth climb flight test Pressure Altitude ft Single engine Temperature Standard
Solution Exercise Climb Given conditions of Saw tooth
climb flight test Pressure Altitude ft Single engine Temperature Standard
Solution Exercise Climb Given conditions of
Solution Exercise Climb
(Solution) 1 Exercise 7: Climb 1. Given conditions of "Saw-tooth" climb flight test. Pressure Altitude-2000 ft Single engine Temperature: Standard...

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need tutor to help with these aircraft performance homework assignments. Must know about aircraft performance equations.1 Exercise 7: Climb 1. Given conditions of “Saw-tooth” climb flight test. Pressure Altitude-2000 ft Weight 300,000 lbs Single engine Method Constant Airspeed Climb +/- 500 ft Temperature: Standard (Climb from 1500 ft to 2500 ft) Assume negligible airspeed errors due to position and compressibility Airspeed Airspeed Climb Time Average Rate of Climb Average Rate of Climb Angle of Climb (KIAS) (KTAS) (s) (ft/min) (kts) (deg) 140 80 160 65 180 60 190 70 Fill out the above table. Find: (a) Indicated Airspeed for Vx (Best Angle Climb Airspeed) and Vy (Best Rate of Climb Airspeed) (b) Angle of Climb for Vx (c) Rate of Climb for Vy (d) Specific Excess Power at Vy (e) Excess Thrust at Vy and Vx This document was developed for online use in ASCI 310. File Name: Exercise_7

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