Explicit equations involving only square root and summation operations are derived for computing barometric altitude from measured data. Three different expressions are obtained for the altitude ranges -1,000 ft to 32,500 ft, 32,500 ft to 45,000 ft, and 45,000 ft to 60,000 ft, which satisfy the accuracy requirements for pressure altitude given in an ARINC specification. Although implementation of the equations would not offer many advantages where advanced digital computation techniques are available, they go along with the equations for Mach number and airspeeds in the explicit forms given by Bogel (1974)
Present day barometric altimeters calculate atmospheric heights by assuming the ICAO (International ...
Vertical navigation is crucial for safe aircraft separation, which have been traditionally based on ...
Detailed tables of pressures and densities are given for altitudes up to 20,000 meters and to 65,000...
Explicit equations involving only square root and summation operations are derived for computing bar...
under research authorization formulated and recommended by the subcommittee on aero-dynamics and app...
Knowledge of standard air temperature, pressure, density, speed of sound, and viscosity as a functio...
During 1925 the assumption of an isothermal atmosphere which was in general use as the standard for ...
erence 1) are reprinted since that report h oti of prini. Adoantage is taken to muke certain rezrkic...
Symbols and definitions of various airspeed terms that have been adopted as standard by the NACA Sub...
The article presents the use of barometric sensors to precisely determine the altitude of a flying o...
MWR-064-03-0069The recently-developed Refsdal "aerogram" possesses the interesting property of provi...
The main task of this paper is to describe altitude measurement methods and specify how to process t...
This report is a revision of the altitude pressure tables of the United States standard atmosphere g...
This report is Section two of a series of reports on aeronautic instruments (Technical Report nos. 1...
Detailed tables of pressures and densities are given for altitudes up to 20,000 metem and to 65,000 ...
Present day barometric altimeters calculate atmospheric heights by assuming the ICAO (International ...
Vertical navigation is crucial for safe aircraft separation, which have been traditionally based on ...
Detailed tables of pressures and densities are given for altitudes up to 20,000 meters and to 65,000...
Explicit equations involving only square root and summation operations are derived for computing bar...
under research authorization formulated and recommended by the subcommittee on aero-dynamics and app...
Knowledge of standard air temperature, pressure, density, speed of sound, and viscosity as a functio...
During 1925 the assumption of an isothermal atmosphere which was in general use as the standard for ...
erence 1) are reprinted since that report h oti of prini. Adoantage is taken to muke certain rezrkic...
Symbols and definitions of various airspeed terms that have been adopted as standard by the NACA Sub...
The article presents the use of barometric sensors to precisely determine the altitude of a flying o...
MWR-064-03-0069The recently-developed Refsdal "aerogram" possesses the interesting property of provi...
The main task of this paper is to describe altitude measurement methods and specify how to process t...
This report is a revision of the altitude pressure tables of the United States standard atmosphere g...
This report is Section two of a series of reports on aeronautic instruments (Technical Report nos. 1...
Detailed tables of pressures and densities are given for altitudes up to 20,000 metem and to 65,000 ...
Present day barometric altimeters calculate atmospheric heights by assuming the ICAO (International ...
Vertical navigation is crucial for safe aircraft separation, which have been traditionally based on ...
Detailed tables of pressures and densities are given for altitudes up to 20,000 meters and to 65,000...