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International standard atmosphere in elevation -2000 to 30000 metre - pressure, temperature, density, viscosity, thermal conductivity and velocity of sound.
- Barometric Pressure
International Standard Atmosphere International standard...
- Elevation
Speed of sound in some gases at zero degrees Celsius and...
- Air Temperature, Pressure and Density Vs. Altitude
Thermal properties of air at different temperatures -...
- Barometric Pressure
Table A–16 Properties of the atmosphere at high altitude Table A–17 Ideal-gas properties of air Table A–18 Ideal-gas properties of nitrogen, N 2 ... Society of Heating, Refrigerating and Air-Conditioning Engineers, Inc., 1993), pp. 16.4 and 36.1. 908 PROPERTY TABLES AND CHARTS
The density of the air for a given level of humidity can be found by applying a correction factor to the above calculated perfect gas density. The correction factor, K h, can be found by using wet and dry bulb temperature measurements to predict relative humidity as shown in the following table.
International Standard Atmosphere. Sea Level Conditions. Property: Metric Value: Imperial Value: Pressure: 101.3 kPa: 2116.2 lb f /ft 2: Density: 1.225 Kg/m 3: 0.002378 slug/ft 3: Temperature
The U.S. Standard Atmosphere is a set of models that define values for atmospheric temperature, density, pressure and other properties over a wide range of altitudes.
Online calculator, figures and tables showing density, specific weight and thermal expansion coefficients of air at temperatures ranging -100 to 1600 °C (-140 to 2900 °F) at atmospheric and higher pressure - Imperial and SI Units.
Prefixes: giga, G = 109 mega, M = 106 kilo, k = 103 nano, n = 10–9 micro, μ = 10–6 milli, m = 10–3. density: water 1000 kg/m3; air 1.2 kg/m3 specific heat: water 4.2 kJ/(kg·K); air 1.0 kJ/(kg · K) Sensible Heat: SH= 1.2 Q∆t. Total Heat: TH = 1.2 Q∆h. Latent Heat: LH = 3.0 Q∆w.
