Tabulated aerodynamic data from coannular nozzle performance tests are given for test runs 26 through 37. The data include nozzle thrust coefficient parameters, nozzle discharge coefficients, and static pressure tap measurements.
Model Aerodynamic Test Results for Two Variable Cycle Engine Coannular Exhaust Systems at Simulated Takeoff and Cruise Conditions. Comprehensive Data Report. Volume 2: Tabulated Aerodynamic Data Book 2
1981
446 pages
Report
No indication
English
Jet & Gas Turbine Engines , Aerodynamic characteristics , Exhaust nozzles , Exhaust systems , Variable cycle engines , Wind tunnel tests , Cruising flight , Deflectors , Ejectors , Irises (Mechanical apertures) , Jet thrust , Nozzle design , Static pressure , Supersonic flight , Tables (Data) , Takeoff