Using shock-expansion cancellation technique flow in the diverging part of a supersonic nozzle is brought back to free stream direction ( direction parallel to the axis of nozzle) where a rhombus shaped region(Test Section) is formed in which uniform flow is ensured. Refer Method Of Characteristics from Rathakrishnan For Diagram.
There is usually an additional throat placed in the tunnel downstream of the test section to shock down the supersonic flow to subsonic. The advantage of a supersonic continuous flow wind tunnel is the longer run times relative to a blowdown tunnel. The major disadvantage is the increased size and operating costs.
To create your own supersonic wind tunnel, you'll need a high-pressure air source, a converging nozzle to accelerate the airflow, and a test section where you can observe the effects of supersonic flow. Start by constructing a chamber that can withstand high pressures and connect it to your nozzle, which should gradually narrow to increase airspeed. Include a diffuser at the exit to help stabilize the flow and a measurement setup with sensors to capture data during your tests. Be sure to follow safety protocols, as working with supersonic speeds can be hazardous.
. Gessner has written: 'The importance of the supersonic wind tunnel in projectile development'
the underground tunnel in goldenrod
Leslie T. Miller has written: 'The supersonic wind tunnel'
Goldenrod's Tunnel
after you get 7 badges, head down to the goldenrod tunnel. talk to everyone it the tunnel. one of them will give you the uniform but you'll lose it as you proceed the storyline
Go to the Underground Tunnel in Goldenrod City. There is a Team Rocket Grunt there who will give you a uniform.
Robert J. Bruckner has written: 'A supersonic tunnel for laser and flow-seeding techniques' -- subject(s): Wind tunnels, Supersonic wind tunnels, Flow visualization
The small size of the working area in a supersonic tunnel is necessary to create the high-speed, high-pressure airflow required for testing at supersonic speeds. Restricting the area helps achieve the desired air velocities and pressures necessary for accurate testing of aerodynamic properties. Additionally, the smaller working area allows for better control and measurement of flow characteristics.
in the underground tunnel in goldenrod
Christopher A. Lee has written: 'Design and testing of an oblique all-wing supersonic transport' -- subject(s): Transport aircraft, Wind tunnel tests, Propulsion system configurations, Oblique wings, Supersonic wind tunnels, Wind tunnel models, Aircraft design, Supersonic transports 'I, digital' -- subject(s): Family archives, Personal archives, Digitization, Digital preservation, Archival materials