My (Spring 2022) Exam 2

Please circel or box final answer and please indicate which part the work is under

subject (fluid mechanic 2) pls show me full steps with clear handwriting sir pls answer within 30 min sir

Given: The plane accelerates in its current trajectory with a= 100 m/s^2 Farag Angle theta= 5° W=105 kips F_drag= 80 kips m= 1000 lbs Find: F_thrust, F_lift Please include the KD. Fthrust Futel t Fueight 000 BY NC SA 2013 Michael Swanbom

Subject: Air Pollution Formation and Control Do not just copy and paster other online answers Correct answer (a) 0.023 psi  ;  (b) 12,000 MW Show step by step soluction

Fluid Mechanics Problem   Note: Fluids are assumed to be at 20oC.

Note:- • Do not provide handwritten solution. Maintain accuracy and quality in your answer. Take care of plagiarism. • Answer completely. • You will get up vote for sure.

Pls help ASAP

Choose the incorrect statement/s about fluid flows. Select the correct response(s): Whenever the flow parameter does not change with distance along the flow path, the fluid flow is uniform It is non-uniform fluid flow when the flow parameters change and are varied at different points in the flow path It may change from point to point (velocity, pressure, cross-section) but not over time with a steady flow. Conditions vary from point to point in the stream, but remain constant over time for a steady non-uniform flow. When the conditions in any part of the fluid are constant over time, the flow is said to be unstable There are two parameters common to all fluid flow: the particle velocity and the fluid pressure.

Find Temperature Ratio at Cruising Altitude. Barometric Altimeter setting = 29.42 in.Hg Cruising Indicated Altitude = 9,500 ft Outside Air Temperature at altitude = 13.34 deg F   0.9120 0.8625 0.2261 0.9312

22°F Clear DDÈ DDE MMMBU BU ► ► ► 2GQ==§¤¤✰=aaa=Û¤ı1 × PDF PDF PDF PDF PDE File | C:/Users/ignor/Downloads/Assignment%203%20(2).pdf T❘ Read aloud Draw Ask Copilot a) Use Newton's second law b) Use the Torque equation a Search TWO Particle P is sliding along a circular path of radius r . The circular path is placed on top of a truck that is moving to the left with a velocity of v and an acceleration of a. The friction is negligible. Find the EOM of particle P. O 0 2 r of 6 | CD P eac СО da | + o ENG 60 T 6L N {0} 7:39 PM 1/17/2024 x

Fluid Mechanics Problem   Note: Fluids are assumed to be at 20oC.

The Reynold's number of a sphere falling in air is 1E6. If the sphere's radius is 1ft, what is its velocity? Density of air is 0.00234 slug/ft³ and viscosity of air is 3.8E-7 lbf-sec/ft²A. 2.5 ft/sB. 5.1 ft/sC. 40.6 ft/sD. 81.2 ft/s

b) Calculate The estimated drag force, D, With Uncertainty. Is it enough to keep a 160lb person floating Hint:Error Propagation The drag force on this skydiver can be calculated by the expression for the drag coefficient: CD = D/((1/2)*pU2A) The Drag Coefficient, CD, is estimated at 1.2 ± 0.1 A, is measured by a camera with image processing. The camera is about ±10% accurate. Measurements for A are Given. Measurements for wind speed, U, were found with an anemometer The temperature of air at was measured with a thermocouple with an uncertainty of  ±2K. temperature is 300k   A (m2) U (m/s)+ 0.651 40.8 0.649 41.0 0.655 40.4 0.654 40.2 0.650 38.9 0.648 39.5 0.645 39.1 0.649 40.6 Anemometer Specs: Measurement Accuracy for air speed: ±(2% + 0.2m/s), ±(2% + 0.8 km/hr), ±(2% 0.4mph), ±(2% + 0.4 knots), ±(2% +40ft/min) Measurement resolution for air speed: 0.1ms, 0.1km/hr, 0.1mph, 0.1 knots, 1.0ft/min

( computational fluid dynamics question) Question:  If the calculations lag behind the flow of fluid, what factor of the simulation gets affected? Circle Final answer or State it clearly