Aeronautical Calculator APK

Download Aeronautical Calculator 1.0.1 APK

App Description

Aeronautical Calculator is malta,aerocalc,tools,aeronautical,calculator, content rating is Everyone (PEGI-3). This app is rated 5 by 1 users who are using this app. To know more about the company/developer, visit Dan Malta website who developed it. malta.aeroCalc.apk apps can be downloaded and installed on Android 1.6 and higher Android devices. The Latest Version of 1.0.1 Available for download. Download the app using your favorite browser and click Install to install the application. Please note that we provide both basic and pure APK files and faster download speeds than APK Mirror. This app APK has been downloaded 3+ times on store. You can also download malta.aeroCalc APK and run it with the popular Android Emulators.

Calculate non standard atmospheric characteristics (according to the 1976 International Standard Atmosphere model), convert various altitude and airspeed types with regard to sea level atmospheric conditions.
Correct up to geometric altitude of 84 kilometers.

Usage:
1) Enter mean sea level characteristics (temperature, pressure).
2) Enter chosen altitude (geometric or geopotential) or gravity, press 'done' and view atmospheric properties at 
chosen altitude \ gravity.
3) Enter chosen airspeed (true or calibrated or equivalent; up to the local value of the speed of sound) or dynamic 
pressure or mach number (up to mach one), press 'done' and view airspeed type converted at current altitude and 
mean sea level characteristics.

Notice: 
1) Long click each variable label to get information regarding that variable.
2) Use right side spinners to change input / output unit types.

Remarks:
1) Airspeed conversion is performed under assumption that air is compressible, isentropic (subsonic; mach
number < 1.0) and dry with a constant specific heat ratio.
2) If at current atmospheric conditions, input airspeed results in mach number greater then 1 - calculation is 
performed according to mach number 1.
3) Density is calculated using a perfect gas relationship.
4) Geopotential altitude input is defined according to standard day (ISA).
5) The mean molecular weight is not corrected for geometric altitude above 80km.

Questions or bug reports? please contact me at [email protected].
 

App ChangeLog

• Fixed a bug preventing mean sea level temperature to be negative.

App Screens