Using the results of linearized theory calculate the lift and wave-drag coefficients for an infinitely thin flat
Question:
Using the results of linearized theory calculate the lift and wave-drag coefficients for an infinitely thin flat plate in a Mach 2.6 free stream at angles of attack of
(a) a = 5°
(b) a = 15°
(c) a = 30°
Compare these approximate results with those from the exact shock-expansion theory obtained in Prob. 9.13. What can you conclude about the accuracy of linearized theory in this case?
Fantastic news! We've Found the answer you've been seeking!
Step by Step Answer:
a a 5 00873 rad C ce 11 4a M 400873 261 01455 From exact theory Prob 913 ce 0148 0148 01455 0148 err...View the full answer
Answered By
Mugdha Sisodiya
My self Mugdha Sisodiya from Chhattisgarh India. I have completed my Bachelors degree in 2015 and My Master in Commerce degree in 2016. I am having expertise in Management, Cost and Finance Accounts. Further I have completed my Chartered Accountant and working as a Professional.
Since 2012 I am providing home tutions.
2+ Reviews
10+ Question Solved
Related Book For 
Question Posted:
