The effects of geometric design parameters on the internal performance of nonaxisymmetric single expansion-ramp nozzles were investigated at nozzle pressure ratios up to approximately 10. Forward-flight (cruise), vectored-thrust, and reversed-thrust nozzle operating modes were investigated.
Static Internal Performance of Single Expansion-Ramp Nozzles with Thrust Vectoring and Reversing
1982
143 pages
Report
No indication
English