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Flugzeuggasturbine
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FULL-SCALE EVALUATION OF SOME FLAMEHOLDER DESIGN CONCEPTS FOR HIGH-INLET-VELOCITY AFTERBURNERS
Foaming characteristics of MIL-L-7808 turbine lubricants
Method of spare parts: Digital simulation of aircraft turbine engine control system
Experimental investigation of two-stage air-cooled turbine suitable for flight at Mach 2.5
Introduction to the Special Section on Recent Progress on Rotating Detonation and Its Application
Impact of the turbulence modeling approach on the accuracy of the fan noise level prediction
Annular Magnetohydrodynamic Physics for Turbojet Energy Bypass
Air force facility for large turbine engine compressor testing
Application of non-afterburning turbojets to supersonic flight
Considerations for using phased array ultrasonics in a fully automated inspection system