Gas turbine combustor Patent
Method for maintaining good performance in gas turbine during air flow distortion
Engineering topics
Publications and source records attributed to Roudebush, W. H..
Method for maintaining good performance in gas turbine during air flow distortion
Shorter combustors for high temperature jet engines of high speed aircraft, considering lifetime, shroud scoops, overheating, warpage, etc
Short annular combustors for high temperature aircraft engines noting test results
State-of-the-art in very short annular combustors for high temperature aircraft engines
Nonsteady heat transfer and flow problem for cylindrical liquid hydrogen tank pressurization during outflow
Aerodynamic heating calculation of Atlas Centaur launch vehicle trajectory
Potential flow theory for two-dimensional cascades, and application to fluid flow through axial flow compressors
Viscous effects on two-dimensional incompressible flow about compressor blade profiles in cascade
Pressurized liquid hydrogen tank outflow analysis
Pressurized liquid hydrogen tank outflow