Nozzle lateral spacing effect on drag and performance of twin jet afterbody configurations with convergent nozzles at Mach 0.6 to 2.2
Effect of Nozzle Lateral Spacing on Afterbody Drag and Performance of Twin-jet Afterbody Models with Convergent Nozzles at Mach Numbers Up to 2.2
1970-10-01
Report
No indication
English