Engineering, 27.10.2021 07:20 hxmiltrxshh
The measured lift slope for the NACA 23012 airfoil is 0.1080 degree−1 , and αL=0 = −1.3 ◦ . Consider a finite wing using this airfoil with AR = 8 and taper ratio of 0.8 which corresponds to τ = 0.054 and e = 0.95. Calculate the lift and induced drag coefficients for this wing at a geometric angle of attack of 3◦ . CL ≈ 0.37 and CDi ≈ 0.006.
Answers: 3
Engineering, 04.07.2019 18:10
Thermal stresses are developed in a metal when its a) initial temperature is changed b) final temperature is changed c) density is changed d) thermal deformation is prevented e) expansion is prevented f) contraction is prevented
Answers: 2
Engineering, 04.07.2019 18:10
At 12 noon, the count in a bacteria culture was 400; at 4: 00 pm the count was 1200 let p(t) denote the bacteria cou population growth law. find: (a) an expression for the bacteria count at any time t (b) the bacteria count at 10 am. (c) the time required for the bacteria count to reach 1800.
Answers: 1
Engineering, 04.07.2019 18:10
Manometers are good examples of measuring instruments, nowadays they are not as common as before. a)-capacitive probe gauges b)-gravitational gauges deformation ) gauges d)-digital gauges
Answers: 1
Engineering, 04.07.2019 18:10
Hydraulic fluid with a sg. of 0.78 is flowing through a 1.5 in. i.d. pipe at 58 gal/min. the fluid has an absolute viscosity of 11.8 x 105 lbf-sec/ft2. is the flow laminar, turbulent or within the critical range? give both a numerical reynolds number and a term answer.
Answers: 3
The measured lift slope for the NACA 23012 airfoil is 0.1080 degree−1 , and αL=0 = −1.3 ◦ . Consider...
Biology, 04.11.2020 19:20
History, 04.11.2020 19:20
Mathematics, 04.11.2020 19:20
Mathematics, 04.11.2020 19:20