A review of lift fan propulsion systems for civil VTOL transports
Lift fan propulsion systems for civil VTOL aircraft
Engineering topics
Publications and source records attributed to Lieblein, S..
Lift fan propulsion systems for civil VTOL aircraft
Problem areas for lift fan propulsion for civil VTOL transports
Radiator heat transfer and geometric characteristics of Brayton space power cycle using gas-solid suspension working fluid
Crater characteristics of 11 metal alloys under hypervelocity impact including effects of projectile density and target temperature
Theoretical analysis of axisymmetric flow in VTOL lift fan inlets without crossflow
Comparative analysis of single-loop 100-kilowatt Brayton space power system using pure gas and gas-solid suspension as working fluids
Weight, heat transfer, and efficiency comparison for Rankine cycle space radiators constructed of three different finned tube geometries
Liquid metal radiator and condenser test facility
Materials and fin tube geometry effects on ultimate size and mass of space radiator
Feasibility studies of space radiators using vapor chamber fins
Heat transfer coefficient, friction factor, and pressure drop analyzed in flow of gas - solid dilute suspension
Heat rejection characteristics of space radiator panels utilizing shared fins
Dimple, spall, and perforation of aluminum, niobium, and steel plates under hypervelocity impact
Feasibility studies of space radiators using vapor chamber fins for application to Rankine system powerplants
Material and geometry aspects of meteoroid armor protection for space radiator tubes, discussing bumper-fin concept
Hypervelocity impacts into space radiator materials, discussing material evaluation for waste heat shield
Photographic meteor data - significance in design of meteoroid protection for large space vehicles
Vapor chamber fin-tube radiator geometries for high power Rankine cycle system on spacecraft