The design of variable Mach number asymmetric supersonic nozzles by two procedures employing inclined and curved sonic lines
Description: Report presenting two theoretical procedures for designing asymmetric supersonic nozzles for which the calculated exit flow is nearly uniform over a range of Mach numbers. One is for Mach numbers less than approximately 3 and one is for Mach numbers greater than 3.
Date: March 1953
Creator: Syvertson, Clarence A. & Savin, Raymond C.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department