National Advisory Committee for Aeronautics (NACA). — Meffet Field, Calif.: Ames Aeronautical Laboratory, 1953. — 73 p.
This report, which is a revision and extension of NACA-TN-1428, presents a compilation of equations, tables, and charts useful in the analysis of high-speed flow of a compressible fluid. The equations provide relations for continuous one-dimensional flow, normal and oblique shock waves, and Prandtl-Meyer expansions for both perfect and imperfect gases. The tables present useful dimensionless ratios for continuous one-dimensional flow and for normal shock waves as functions of Mach number for air considered as a perfect gas. One series of charts presents the characteristics of the flow of air (considered a perfect gas) for oblique shock waves and for cones in a supersonic air stream. A second series shows the effects of caloric imperfections on continuous one-dimensional flow and on the flow through normal and oblique shock waves.
Contents:SummaryIntroductionSymbols and notationFundamental relationsThermodynamicsThermal equations of state
Caloric equation of state
Energy relations
Specific heats
Enthalpy
Entropy
Continuous one-dimensional flowBasic equations and definitions
Integrated forms of energy equation
Pressure-density relation
Bernoulli's equation
Relations between local and free-stream conditions
Useful ratios
Stream-tube-area relations
Shock wavesNormal shock wavesBasic equations
Useful relations
Oblique shock wavesBasic equations
Connection with normal shock
Useful relations
Shock polar
Supersonic flow past wedges and conesFlow past wedgesFlow past conesPrandtl-Meyer expansionImperfect-gas effectsThermodynamicsEquations of state
Specific heats
Continuous one-dimensional flowBasic equations and definitions
Integrated forms of energy equation
Pressure and density relations
Stream-tube-area relations
Normal shock wavesOblique shock wavesPrandtl-Meyer expansionAppendicesViscosity and thermodynamic constants for air
Reynolds number
Pressure conversion factors
ReferencesTablesCharts