-
The reservoir of a supersonic wind-tunnel has a total temperature and total pressure of \(600\,K\) and \(11\,atm\). If the flow …
- 439 views
- 1 answers
- 0 votes
-
Find the enthalpy change, internal energy change and entropy change across a shock wave whose upstream air temperature and pressure …
- 517 views
- 1 answers
- 0 votes
-
Find the reservoir pressure for a nozzle of a supersonic wind tunnel which has an exit-to-throat area ratio of \(4.441\). …
- 361 views
- 1 answers
- 0 votes
-
Find the lift and wave drag coefficients for an infinitely thin flat plate at an angle of attack of \(8^{\circ}\) …
- 411 views
- 1 answers
- 0 votes
-
An oblique shock wave is generated with a wave angle of \({30^ \circ }\) in a Mach \(4\) flow, at …
- 512 views
- 1 answers
- 0 votes
-
A flow passes through a normal shock wave has a pressure, temperature and Mach number of \(1\,atm,\,295\,K\) and \(2.8\) upstream …
- 324 views
- 1 answers
- 0 votes
-
What are expansion waves ? How does it originates ?
- 759 views
- 1 answers
- 0 votes
-
What are shock waves ? How does it originates ?
- 625 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 …
- 733 views
- 1 answers
- 0 votes
-
What is a Mach wave ? How does it forms ?
- 615 views
- 1 answers
- 0 votes
©2022 aerospaceanswers.com
Terms & Privacy
Terms & Privacy
Question Tag: Supersonic flow
Filter by
Filter by
Questions Per Page:
