Investigation of heat transfer and pressure on flat plates and curved panels due to rocket exhaust impingement
Pressures and heat transfer rate predictions for rocket exhaust impingement on flat plates and curved panels
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Pressures and heat transfer rate predictions for rocket exhaust impingement on flat plates and curved panels
Design and performance study of flat plate thermoelectric generators for solar probes
Hydraulic flow approximation for flow induced vibration analysis on flat plate suspended in narrow channel
Finite Mach number effect on self induced weak interaction pressures on flat plate
Radiation transfer effect on equilibrium temperature for laminar boundary layer flow of absorbing-emitting gas over flat plate
Transpiration cooling of porous flat plate by injection of carbon dioxide or air into carbon dioxide and air free streams
Unsteady compressible boundary layer flow over flat plate whose temperature is varied with time
Flat plate thermoelectric generators for solar probe missions
Computer program calculates the stresses and lateral deflections to a uniform thickness flat plate with a uniform pressure load. The plate to be analyzed may have several different boundary conditions. The program is written in FORTRAN 4 for use on the CDC 6600 computer.
Two tools facilitate chemical stripping of insulation on flat conductor cabling. A tape pressing tool and a taping fixture apply adhesive lead tape with the proper amount of pressure to protect the remaining insulation from the chemical stripping solution.
To improve shielding of flat multicore cables, a thin, seamless ferrous shield around all cores optimizes low frequency magnetic shielding. Such shielding is covered with an ultrathin seamless coat of highly conductive nonferrous material.
Moire tester detects small variations in flat conductor cable spacing by a quick, visual inspection. This device compares the cable to be tested with the negative of a very precise standard cable. The moire, consisting of bands of light and dark zones and its irregularities, can be interpreted as errors in spacing.
Hypersonic turbulent boundary layers on flat plates and delta wings
Heat transfer and pressure distribution due to two-dimensional repetitive sine wave distortions on flat plate at Mach 20 in helium
Stiffness matrices analysis of thin flat plates
Three dimensional incompressible wake behind blunt obstacle located at leading edge of flat plate
Leading edge effects on laminar flat-plate boundary layer at Mach 10.4
Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.4