Additional experiments with flat-top wing- body combinations at high supersonic speeds
Flat top wing body configuration effects on aerodynamic characteristics of supersonic aircraft
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Flat top wing body configuration effects on aerodynamic characteristics of supersonic aircraft
Material properties, shielding, and coatings examined in development of flat flexible conductor cables
Fortran IV program manual for computing flutter boundaries of flat panel arrays in supersonic flow
Measurement of compressible turbulent boundary layer skin friction on porous flat plate with mass injection
Steady state thermal conductance coefficient at interface formed by nominally-flat rough contacting surface placed in vacuum environment
Stick module interconnection of flat packs into single-axis motherboard
Mass evaporation rate and heat transfer coefficients for water drops supported by own superheated vapor over flat plate
Mass evaporation rate and heat transfer coefficients for water drops supported by own superheated vapor over flat plate
Multiple element continuity gage measures plane stress crack growth plus surface crack growth under plane strain conditions. The gage measures flat and curved surfaces and operates at cryogenic temperatures.
Polymer adhesive laminates polyimide-film flat conductor cable. It is obtained by reacting an appropriate diamine with a dianhydride. The adhesive has also been used in the lamination of copper to copper for the preparation of multilayer circuit boards.
Flat pack interconnection structure composed of stick modules simplifies modular electronic assemblies by allowing a single axis mother board. Two of the wiring planes are located in the stick module, which is the lower level of assembly, with the third wiring plane in the mother board.
Crack propagation measurement by foil strain gauge on flat and curved surfaces at cryogenic temperatures
Maximum lift-drag ratio of slender, flat top, hypersonic body assuming modified Newtonian pressure distribution and constant surface averaged skin friction coefficient
Effect of Reynolds number on slosh damping by flat ring baffles
Flutter analysis of flat rectangular panels based on three-dimensional supersonic unsteady potential flow
Solar pressure perturbation effects on orbit of flat reflecting satellite
Reynolds number and flow incidence effects on cross flow characteristics of flat front, two- dimensional cylinders
Packaging methods for electronic components encased in flat pack geometries, and spacecraft applications of proposed methods