Exploratory study of open-face honeycomb to reduce temperature of hypersonic aircraft structure
Wind tunnel study of open-face honeycomb to reduce temperature of hypersonic aircraft structure
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Wind tunnel study of open-face honeycomb to reduce temperature of hypersonic aircraft structure
Dynamic and interfacial fluid effects in mechanical face seals, discussing hydrodynamic pressure generation
Orifice compensated hydrostatic face seal under pressure and thermal loading for aircraft gas turbine
Nondestructive tests for determining braze bond quality of open face honeycomb seal rings, using low viscosity liquids with fluorescent additives
Misalignment and eccentricity effect on face seal, discussing leakage dependence on phase angle
Eccentric face seal with tangentially varying film thickness, analyzing leakage flow proportional to eccentricity and surface waviness
Face seals for jet engine mainshaft bearing compartments, emphasizing oil film and gas film seals
Gas turbine engine shaft face seal with self acting lift augmentation preventing rubbing contact, noting disadvantages of labyrinth and conventional seals
Leakage in mechanical face seals with hydrodynamic films, noting misaligned seal theories for pumping with cavities and two fluids
General computer program for calculating axisymmetric temperature field applied to gas turbine face seal thermal deformation
Leakage in mechanical face seals with hydrodynamic films, noting misaligned seal theories for pumping with cavities and two fluids
Misalignment and eccentricity effect on face seal, discussing leakage dependence on phase angle
Eccentric face seal with tangentially varying film thickness, analyzing leakage flow proportional to eccentricity and surface waviness
Intensity and velocity distributions of thermal energy argon atoms scattered from silver /111/ face, using time of flight methods
Dielectric covered narrow radiating slots in rectangular waveguide broad face, calculating impedance from equivalent circuits
Sealing dam analysis for design of shaft face seal with self-acting lift augmentation for advanced gas turbine engines
Integral analysis of heat transfer downstream of rearward-facing step with small coolant injection
Measurement of flow distribution caused by forward facing nozzles exhausting near large cylindrical body at hypersonic speed