Only (a) part needs to be solved. 8.This question is based around an aircraft with the following characteristics:CD0.04 + 0.025 C?Weight200 kNWing area75 m2For this part only, assume the aircraft has a turboprop propulsionsystem that has 5 MW of available power at sea level. What is the(a)maximum climb rate of the aircraft at sea level and at what climb angleis this rate of climb achieved?(b)The aircraft performs a constant speed, powered descent at anequivalent air speed of 160 m s-1. The descent angle, the angle thedirection of motion makes with the horizontal, is 12°. How much thrustis required to maintain constant speed?(c)For this part only, assume the aircraft has a turbojet propulsion systemthat has 80 kN of thrust available at sea level and thrust available isproportional to density. The aircraft is required to climb at a constantangle of 15°. What is the highest altitude that this climb angle can beachieved?

Answered: Image /qna-images/answer/eba33824-348a-469c-b04b-19f30165f708.jpg

8. This question is based around an aircraft with the following characteristics: Co = 0.04 + 0.025 c? Weight Wing area 200 KN 75 m2 (a) For this part only, assume the aircraft has a turboprop propulsion system that has 5 MW of available power at sea level. What is the maximum climb rate of the aircraft at sea level and at what climb angle is this rate of climb achieved?

8. This question is based around an aircraft with the following characteristics: Co = 0.04 + 0.025 c? Weight Wing area 200 KN 75 m2 (a) For this part only, assume the aircraft has a turboprop propulsion system that has 5 MW of available power at sea level. What is the maximum climb rate of the aircraft at sea level and at what climb angle is this rate of climb achieved?

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

See similar textbooks

Similar questions

6,000 ft of 7-in C-75 grade of casing string will be run in a borehole having a diameter of 8.5-m. The casing has a unit weight of 38 lbm/ft and a wall thickness of 0.540-in. Mud weight used to run the casing into the borehole is 10 lbm/gal (ppg). a) Calculate the weight of casing string in the air. b) Calculate the hook load when the casing is in the borehole. c) Calculate the borehole capacity in terms of bbl/ft. d) Calculate the borehole capacity in terms of bbl. e) Calculate the displacement of the casing in terms of bbl/ft. ) Calculate the displacement of the casing in terms of bbl, g) Calculate the volume of cement slurry to fill the annulus in terms of bbl and cuft assuming a excess volume factor of 1.5) h) Calculate the maximum length of the casing if the rig used for this operation can handle 250,000 Ibf of hook load. i) The casing gets stuck at bottom of the borehole while running the string. Calculate the maximum pulling force that the driller can apply at the surface to get…
Q.2 Four cars, with a mass of 1500 kg each, are loaded on a 6 m wide, 12 m long small car ferry. How deep, in cm will it sink in the water? A 15.2 В 11.5 C 10.2 D 8.3
LR = 5m, LG = 2.5m and LC = 1.1m Q2. The Skylark family of sounding rockets consisted of a number of variants (denoted Skylark 5, Skylark 7, and Skylark 12 respectively). These are illustrated on Page 3. The data given below is based on that for the rocket motors they used (all manufactured and named by what was Royal Ordinance – now part of Roxel): Raven XI Motor Total mass: 1280 kg Length = LR See Case Table (units are m) Diameter = 0.44 m Goldfinch IIA Motor Total mass: 420 kg Length = LG See Case Table (units are m) Diameter = 0.44 m Cuckoo IV Motor Total mass: 242 kg Length = LC See Case Table (units are m) Diameter = 0.44 m The payload mass which is additional to the motor masses is to be taken as 100 kg. (a) For the configurations of the three rockets shown on Page 3 in Fig. Q2: (i) Determine the Pitching/Yawing moment of inertia of each rocket about the base of each rocket. (ii) Explain how you could then find the the Pitching/Yawing moment of inertia of each rocket about its…
An ion-engine-propelled spacecraft has mass 1000 kg without propellant. Its propellant tank is filled with 30 kg of compressed xenon. If the ion engine is operated on orbit at specific impulse 3000 s, what total AVv (in m/s) is available for the mission? (Use 9.81 m/s? as Earth's sea-level gravity.) (m/s)
If the piston mass is 20 kg and the car mass with its base is 400 kg, what will the minimum pressure (kpa) that is required from the air compressor to lift the car? There are three layers of oils with different specific gravities as S1%30.95, S2%3D0.85, and S3-D0.21. Neglect the shear force between the piston and its cylinder. Control valve piston Air pressure from compressor 25-cm diameter 60 cm S3 S2 50 cm Air S1 40 cm S1
Aircraft B Gross weight 1,600 lb Wing Area 250 ft Maximum thrust 0.011 DO K 0.022 1.45 max Mdr NB 1 mph = 5,280 ft/3,600s = 1 4667 ft/s Aircraft B is a sailplane. Find the maximum-endurance performance and conditions (velocity, glide angle. rate of descent) at 30,000 ft. And calculate the distance (miles) and time (hour) taken to reach sea level under these conditions
Drop-load (I)This exercise is part of a series of problems aimed at modeling a situation by progressively refining our model to take into account more and more parameters. This progressive approach is very close to what professional scientists do! context We want to lower a suspended load in a controlled way, so that it hits the ground with a speed whose modulus is not too great. To do this, the suspended load (B) is connected by a rope passing through a pulley to another mass (A), which can move on a horizontal surface. To slow down the descent, we added a spring behind the mass (A). Information The masses of the charges A and B are known.The mass of the rope itself is negligible (very small compared to the loads).The pulley has negligible mass and can rotate without friction.The charge ? is initially stationary and is at a known height h.The surface on which mass A is placed is horizontal.There is no friction between mass A and the surface on which it is placed.The string attached…
The two following 2 energy level systems (E; = 0 & E; = 1) are brought into thermal contact: System A: 8 distinguishable particles; UA = 4 System B: 4 distinguishable particles; UB = 1 If a single unit of energy transfers from System A to System B, what is the final Wtot for the combined system?
P1.) A closed cylindrical tank 1.5 m in diameter and 4 m long is completely filled with gasoline (sp.gr. = 0.82) and accelerated horizontally at 3 m/s². Find the total force acting at the rear wall and at the front wall of the tank. Find also the accelerating force on the fluid mass. Answer: 10.66 kN and F = 17.36 kN Subject: Fluid Mechanic Lesson: Relative Equilibrium of Liquids Fundamentals of Fluid Flow
4. If the modulus of elasticity (E) for water is given to be 2.2GPa, what pressure is required to reduce the volume by 0.6%? 5. A tank contains two substance oil (A) and water (B) subject to variable air pressure: the dimension is shown below and corresponds to 1atm If air is
:06 Escape from a Sinking Car Assume you are in a car that ran into water and is sinking. The car door is 43 inches wide and 24 inches tall. Assuming you can push 90 lbs at 28 inches from the door hinge. At what water height on the door would you be unable to open the door? Use Weight Density of water = 64 lbs/ft³. Water Height = in.
Drop-load (I)This exercise is part of a series of problems aimed at modelling a situation by progressively refining our model to consider more and more parameters. This progressive approach is very close to what professional scientists do! Context We want to lower a suspended load in a controlled way so that it hits the ground with a speed whose modulus is not too great. To do this, the suspended load (B) is connected by a rope passing through a pulley to another mass (A), which can move on a horizontal surface. Information The masses of the charges A and B are known.The pulley is a ring of mass mp and radius R that can rotate without friction.The surface on which mass A is placed is horizontal.There is no friction between mass A and the surface on which it is placed.The string attached to mass A is perfectly parallel to the surface on which the mass rests. SchematizationDraw a diagram of each object that interests us. Draw x- and y-axes for each object. Draw and name each force…