diff_months: 19

Reynold's Number-Fluid Mechanics Assignment

Flat 50% Off Order New Solution
Added on: 2022-12-29 10:00:06
Order Code:
Question Task Id: 0

P5 (20 pts): A diamond wedge with a thickness ratio of 0.07 and a chord length of 1.5m is placed in a free stream of standard sea-level air of Mach 2.5 at an AOA of 5o. Calculate the lift and drag coefficients of the airfoil using the linearized theory. Also, calculate the contribution of the skin friction on the bottom-rear segment of the airfoil to the drag coefficient of the airfoil. Note: for a flat plate of chord c placed at zero-AOA in a free stream of supersonic M., assume a linear relation between Cpr Re, vs. M- that starts at M-0 and has a slope of -0.0505. Cor is the drag coefficient for one side of the plate and Rec is the Reynolds number based on chord c. Take the viscosity at 1.7894e-5Pa's.

  • Uploaded By : Katthy Wills
  • Posted on : December 29th, 2022
  • Downloads : 0
  • Views : 181

Order New Solution

Can't find what you're looking for?

Whatsapp Tap to ChatGet instant assistance

Choose a Plan


80 USD
  • All in Gold, plus:
  • 30-minute live one-to-one session with an expert
    • Understanding Marking Rubric
    • Understanding task requirements
    • Structuring & Formatting
    • Referencing & Citing


30 50 USD
  • Get the Full Used Solution
    (Solution is already submitted and 100% plagiarised.
    Can only be used for reference purposes)
Save 33%


20 USD
  • Journals
  • Peer-Reviewed Articles
  • Books
  • Various other Data Sources – ProQuest, Informit, Scopus, Academic Search Complete, EBSCO, Exerpta Medica Database, and more