Problem 2: Aircraft Pressure Now consider the door to the A330. Assume the door is 3.0 ft wide and 6.0 ft tall, measured from the top edge straight down to the bottom edge. Its radius of 6.0 ft matches the aircraft body. The airline pressurizes the cabin to ICAO standard pressure at 5,000 ft. The aircraft cruises at an elevation of 40,000 ft. Hint, see Canvas, Week 1, Fluid Property Tables. Part A What is the magnitude of the resultant horizontal hydrostatic force on the door? [lb] Part B What is the location of the resultant hydrostatic force on the door?

Problem 2: Aircraft Pressure Now consider the door to the A330. Assume the door is 3.0 ft wide and 6.0 ft tall, measured from the top edge straight down to the bottom edge. Its radius of 6.0 ft matches the aircraft body. The airline pressurizes the cabin to ICAO standard pressure at 5,000 ft. The aircraft cruises at an elevation of 40,000 ft. Hint, see Canvas, Week 1, Fluid Property Tables. Part A What is the magnitude of the resultant horizontal hydrostatic force on the door? [lb] Part B What is the location of the resultant hydrostatic force on the door?

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

Q/ From the table of water properties at average temperature T, find the water properties: density p, viscosity µ. Then calculate: The cross section area of chamber A= T/4 d2 (cm2 ) The pressure difference along L AP=p g h (atom) Volumetric flow rate q=Q/t (cm3 /s) and finally calculated permeability (Darcy D) qul ΑΔΡ Repeat these reading three time and then find the average of permeability. The informations are : D = 9.9 cm L = 25 cm T= 22 °C V (cc) 600 t (sec) 187 H1 (cm) 108 3 H2 (cm) No 1 2 600 176 109 4 3 600 184 107 3
A certain gas at temperature equivalent to 24 degrees Celsius at 10 cu.m and 160 kPa is compressed to 2.5 cu.m, what is the resulting pressure assuming isothermal conditions in kPa abs? (UP TO THREE DECIMAL PLACES ONLY)
In figure 3 Sgi ; 0.85, Sgz ; 1, h2 ; 98 mm, hi ; 159 mm. Calculate PA in mmhg gage, if the barometer reading is 729 mmhg, what is PA in mmH20 absolute?
TOPIC: BERNOULLI'S THEOREM A cylindrical container with a diameter of 11.5 m. It has an outlet almost to the bottom, rounded (without friction) of 1.2m in diameter. The top of the container is open to the atmosphere. When the level in the container is 12m above the center line of the outlet, how fast does the level fall in the container?
What will be the diameter (in mm) of a water droplet, the pressure inside which is 0.00181 N/cm² greater than the outside pressure? (Take surface tension as 0.075 N/m)
Include a diagram to show analysis (FBD)
A 2 m x 2m x 2m cube (specific weight = 5800 N/m³) floats in a tank of oil and water. (SGoil = 0.8, yw-9810 N/m³) | Th=2 1m a) How much of the cube extends above the oil surface? 4 m water
please solve the termodynamcis question. NOTE: PREVIOUS QUESTİON HAS AN ERROR WİTH THE EQUATION OF P P=C.(V^(1/3)) AS INDICATED IN THE PHOTO.
(b) A Formula 1 team tests their car in a wind tunnel at a scale of 50%, at a speed of Vwinarunnet = 50 m/s. The measured downforce at this speed is Foownforce.WT = 3000 N and the model reference area is Aref wT = 0.5 m?. 1. Find the downforce magnitude on the full-scale race car at the same Reynolds number. Assume constant air density p = 1.2 kg/m. II. It is said that F1 cars could travel upside down, as shown below. At what speed should the full-scale car travel to achieve this, if its mass is m = 740 kg? The acceleration of gravity is g = 9.81 m/s?. Downforce Weight
C1 (a). A lubricating oil having the dynamic viscosity of 0.056 poise and specific gravity of 1.17. Calculate (i) the density of oil in kg/m3, (ii) the weight density of oil in N/m3, (iii) the kinematic viscosity in stokes, and (iv) the specific volume in m3/kg. C1 (b). The capillary effect in a glass tube of 2.8 mm diameter, when immersed in (1) water and (2) mercury are 7.7 mm and -3.5 mm respectively. Calculate the value of surface tension in contact with air for water and mercury in N/m. Take, the contact angle for water =0° and mercury =130°. C1(a). (i).the density of oil in kg/m3 C1(a). (ii) the weight density of oil in N/m3 C1(a). (iii) the kinematic viscosity in stokes C1(a). (iv) the specific volume in m3/kg C1 (b). 1.the value of surface tension (water) in N/m C1 (b). 2. the value of surface tension (mercury) in N/m
What will be the diameter (in mm) of a water droplet, the pressure inside which is 0.00221 N/cm2 greater than the outside pressure? (Take surface tension as 0.075 N/m)
Fluid 10