Tables of Mach number from 0 to 100 for compressible gases with specific heat ratios from 1.66 through 1.10
Mach numbers from 0 to 100 for compressible gases with specific heat ratios 1.66 to 1.10 - table
TABLE↗
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Adiabatic heating and temperature-recovery factor of tubes carrying liquids of high Prandtl number.
Adiabatic heating and temperature recovery factor of tubes carrying liquids of high Prandtl number
PRANDTL NUMBER↗
Heat transfer measurements from a partially dissociated gas with high Lewis number.
Convective heat transfer measurements for partially dissociated carbon monoxide and hydrogen with high Lewis number
LEWIS NUMBER↗
Heat capacity and the Lewis number of a reacting gas.
Heat capacity expression due to chemical reaction, relating composition variations and binary diffusion coefficient with Lewis number, presenting integral equation for system enthalpy
DIFFUSION COEFFICIENT↗
Laminar flow past a sphere at high Mach number.
Laminar hypersonic flow past sphere based on constant-density approximation, solving Navier- Stokes equations and comparing with values of shock Reynolds number
LAMINAR FLOW↗
Heat-transfer measurements on a flat plate with attached protuberances in a turbulent boundary layer at Mach numbers of 2.49, 3.51, and 4.44
Heat transfer measurements on flat plate with attached protuberances in turbulent boundary layer at specified free stream Mach numbers
HEAT TRANSFER↗
Effect of Reynolds number on slosh damping by flat ring baffles
Effect of Reynolds number on slosh damping by flat ring baffles
BAFFLE↗
Experimental performance evaluation of a 4.59- inch radial-inflow turbine over a range of Reynolds number
Effect of Reynolds number on performance of 4.59-inch tip diameter radial inflow turbine
REYNOLDS NUMBER↗
Effects of Reynolds number and flow incidence on the force characteristics of a family of flat-front cylinders
Reynolds number and flow incidence effects on cross flow characteristics of flat front, two- dimensional cylinders
CYLINDER↗
Some effects of Mach number and geometry on sonic boom
Mach number and geometry effects on level of sonic boom overpressure and applicability of Whitham theory to calculation of sonic boom
MACH NUMBER↗
Heat transfer measurements from a partially dissociated gas with high Lewis number.
Convective heat transfer measurements for partially dissociated carbon monoxide and hydrogen with high Lewis number
LEWIS NUMBER↗
Reynolds number and incidence-angle effects on inducer cavitation.
Reynolds number and incidence angle effects on inducer cavitation in water
WATER FLOW↗
Journal-bearing velocity profiles for small- eccentricity and moderate modified Reynolds numbers.
Velocity profiles for infinite cylindrical journal bearing, using small eccentricity perturbation calculation and modified Reynolds number as parameter
REYNOLDS NUMBER↗
Boundary layer transition at hypersonic Mach numbers.
Transition from laminar to turbulent boundary layer flow at hypersonic Mach numbers, noting measurement techniques
TRANSITION POINT↗
Transition measurements at hypersonic Mach numbers.
Boundary layer transition measurements of contoured nozzle flow at hypersonic Mach numbers
HYPERSONIC FLOW↗
Angular distribution of flow from orifices and tubes at high Knudsen numbers.
Cesium vapor flow from orifices and tubes into vacuum analyzed, noting dependence of angular distribution and center line intensity on Knudsen numbers
KNUDSEN NUMBER↗
The cyclotomic numbers of order eighteen with applications to difference sets.
Cyclotomic numbers of order 18 with applications to difference sets
NUMBER THEORY↗
Experimental shock-tube investigation of conditions behind incident and reflected shocks in air for shock Mach numbers between 8.5 and 16.5.
Incident and reflected shocks from laminar and turbulent boundary layers measured over various Mach numbers
WAVE REFLECTION↗