-
What are jet engine and scramjet engine ?
- 59 views
- 0 answers
- 0 votes
-
The reservoir of a supersonic wind-tunnel has a total temperature and total pressure of \(600\,K\) and \(11\,atm\). If the flow …
- 165 views
- 1 answers
- 0 votes
-
Find the lift and wave drag coefficients for an infinitely thin flat plate at an angle of attack of \(8^{\circ}\) …
- 137 views
- 1 answers
- 0 votes
-
An oblique shock wave is generated at a compression corner having a deflection angle of \(20^{^{\circ}}\). The oblique shock wave …
- 174 views
- 1 answers
- 0 votes
-
What are expansion waves ? How does it originates ?
- 233 views
- 1 answers
- 0 votes
-
What are shock waves ? How does it originates ?
- 227 views
- 1 answers
- 0 votes
-
Calculate the wave drag on the wings of an airplane which is flying at a Mach number of \(2.1\) at …
- 235 views
- 1 answers
- 0 votes
-
What is a Mach wave ? How does it forms ?
- 238 views
- 1 answers
- 0 votes
-
An airplane flying at a Mach number of 2.2 makes a Mach wave at the nose. What angle does it …
- 201 views
- 1 answers
- 0 votes
-
What is swept wing ? How does wing sweep affects aircraft performance ?
- 307 views
- 1 answers
- 0 votes
©2021 aerospaceanswers.com
Terms & Privacy
Terms & Privacy
Question Tag: Supersonic airplanes
Filter by
Filter by
Questions Per Page:
-
LATEST QUESTIONS
-
What are the roles of ailerons and flaps in an aircraft?
-
Find the location of this tap on cylindrical surface such that there is no deflection of fluid in the manometer.
-
Find and compare the lift slopes for a straight wing and a swept wing with a half-chord line sweep of \(30^{\circ}\).
-
Considering, \(\tau = 0.1\), find the angle of attack for the wing. Also, find the induced drag for the airplane, if span efficiency factor is \(0.6\).
-
-