NUMERICAL SIMULATION OF TURBULENT SHOCKINDUCED SEPARATED FLOWS: APPLICATION TO THE SUPERSONIC OVEREXPANDED NOZZLE FLOW,Used

NUMERICAL SIMULATION OF TURBULENT SHOCKINDUCED SEPARATED FLOWS: APPLICATION TO THE SUPERSONIC OVEREXPANDED NOZZLE FLOW,Used

In Stock
SKU: DADAX3844318569
Brand: LAP Lambert Academic Publishing
Sale price$139.24 Regular price$198.91
Save $59.67
Quantity
Add to wishlist
Add to compare

Processing time: 1-3 days

US Orders Ships in: 3-5 days

International Orders Ships in: 8-12 days

Return Policy: 15-days return on defective items

Payment Option
Payment Methods

Help

If you have any questions, you are always welcome to contact us. We'll get back to you as soon as possible, withing 24 hours on weekdays.

Customer service

All questions about your order, return and delivery must be sent to our customer service team by e-mail at yourstore@yourdomain.com

Sale & Press

If you are interested in selling our products, need more information about our brand or wish to make a collaboration, please contact us at press@yourdomain.com

Shockinduced flow separation and its subsequent reattachment are encountered in many configurations, such as supersonic inlets or rocket nozzles. These phenomena involve complex interactions of boundary layers with compression or expansion waves and exhibit a lowfrequency unsteady behaviour which still requires a clear explanation. This study aims at better identifying the physical mechanisms which drive the global structure of these flows and suggesting improved numerical tools in order to predict these more accurately. The appearance of free and restricted separations in supersonic separated jets is more particularly investigated. Various hypotheses are tested to explain the evolution of the associated unsteady asymmetric wall pressure field in function of the nozzle pressure ratio. New numerical strategies are proposed and lead to identify more accurately the appearance of free and restricted separations and the timevarying morphology of the flow during the transition process. Possible origins of sideload activities are extensively investigated by performing the azimuthal expansion of wall pressure field.

⚠️ WARNING (California Proposition 65):

This product may contain chemicals known to the State of California to cause cancer, birth defects, or other reproductive harm.

For more information, please visit www.P65Warnings.ca.gov.

Recently Viewed