Engineering, 28.03.2020 02:58 samara49
Consider a rectangular wing mounted in a low-speed wind tunnel. The wing model completely spans the test section so that the flow is essentially two-dimensional. If the wing has an NACA 4415 airfoil section and a chord of 0.3 meters, calculate the lift, drag, and pitching moment about the quarter-chord per unit span when the pressure, temperature, and velocity are 1 atm., 303K, and 42 m/sec., respectively. The angle of attack is 8°. What is the moment about the leading edge for these conditions?
Answers: 3
Another question on Engineering
Engineering, 04.07.2019 18:10
Aflywheel accelerates for 5 seconds at 2 rad/s2 from a speed of 20 rpm. determine the total number of revolutions of the flywheel during the period of its acceleration. a.5.65 b.8.43 c. 723 d.6.86
Answers: 2
Engineering, 04.07.2019 18:10
During a steady flow process, the change of energy with respect to time is zero. a)- true b)- false
Answers: 2
Engineering, 04.07.2019 18:10
Water at the rate of 1 kg/s is forced through a tube with a 2.5 cm inner diameter. the inlet water temperature is 15°c, and the outlet water temperature is 50°c. the tube wall temperature is 14°c higher than the local water temperature all along the length of the tube. what is the length of the tube?
Answers: 3
Engineering, 04.07.2019 18:20
Have a greater impact on maintenance productivity than any other support group. (clo5) a)-the top management b)-inventory and purchasing c)-sub-contracting d)-cmms
Answers: 2
You know the right answer?
Consider a rectangular wing mounted in a low-speed wind tunnel. The wing model completely spans the...
Questions
Mathematics, 01.10.2019 12:00
Physics, 01.10.2019 12:00
Mathematics, 01.10.2019 12:00
Physics, 01.10.2019 12:00
History, 01.10.2019 12:00
Mathematics, 01.10.2019 12:00
Mathematics, 01.10.2019 12:00
Chemistry, 01.10.2019 12:00
Mathematics, 01.10.2019 12:00
Physics, 01.10.2019 12:00
