1976 Standard Atmosphere Calculations Help - Page 2

Wind & Time-Speed-Distance

Weight & Balance

Radius of Action

Miscellaneous Calculations

Temperature Altitude Correction for Pressure Altitude Pressure Altitude QNH QFE Density Altitude Coud Base True Altitude True Airspeed Temperature Rise Mach Number Equivalent Airspeed

Magnetic Course Magnetic Heading Compass Heading True Heading Wind Triangle (TAS - HDG; GS - CRS; WS - WD) Cross / Head Wind Components Time - Speed - Distance Fuel - Time - Fuel Flow

Weight & Balance Sheet CG Shift CG % Aft of MAC CG from Datum Ballast Cargo Pallet Load

Intercepting Moving Target RA - Returning to the Same Base RA - Returning to Alternate Base RA - Returning to Moving Base RA - Returning to Moving Alternate Base

Climb & Descent Gradient Gliding Distance & Glide Ratio Rate of Turn Bank Angle Load Factor Pivotal Altitude Off-Course Problems Time to VOR Distance from VOR

1976 Standard Atmosphere Properties 1976 Standard Atmosphere Graphs

Weight & Force Mass Distance & Length Temperature Time Speed Pressure & Load Volume Area Power Energy & Work Flow (Volume) Flow (Mass) Angle Acceleration

About luizmonteiro.com Mission Statement Executive Staff Contact Us

Flash Clocks for Your Site Flash Instrument Simulator for Your Site

	Surf with confidence! Site has been tested by:
		Norton™ Safe Web
		McAfee SiteAdvisor ®

1976 Standard Atmosphere Help		Your source for:
		Online Aviation Instrument Simulators + E6b, CR3 and other Flight Computer Calculators

Back to calculator |

2

Using the Standard Atmosphere Calculator (Continued...)

Example 2:
In Standard Atmosphere at what altitude is the pressure half of that at sea level? What is the temperature and pressure at that altitude?

The pressure ratio is the ratio between air pressure at a certain altitude and the sea level pressure. The ratio for the pressure to be half, or 50%, will be 0.50. Lets select the pressure ratio field and highlight it with the mouse.

Next, type in the 0.50 value.

As you finish entering the value, all the other properties are calculated for you, including the:

	a -	Altitude in feet which is 17985.6 or about 18,000 feet
	b -	The temperature in Celsius is -20.6021 ^oC or rounded up -21 ^oC.
	c -	The air pressure is 1.49606e+1 inHg or approximately 15 inHg.

In this case we entered data in the Pressure Ratio field, however you can enter information in ANY field, and as long as it is within the range or envelope of Standard Atmosphere. This means that you actually have 378 function combinations on this caluclator!

Back to calculator |

2

	Navigation Simulator
	Practice in our simulator specifically designed for learning the basics of instrument navigation. Try the Navigation Simulator, available for Windows PC. Now completely free. There is also an online version that runs directly on this website, and can be viewed on a Windows PC, Mac, or Linux OS. Note: the Windows PC version of the simulator has its own self-contained Flash, so it works without Flash being installed and is not subject to the Adobe Flash discontnuation / end of life.

Free Online Simulators
No installation required. These simulators are ready to run on your web browser and have a rich set of features. Practice basic VOR, ADF, RMI and HSI intrument orientation and execute holding patterns. Other simulators include pitot static system and altimeter errors. Click here to go to main online simulator page.

All rights reserved to Luiz Roberto Monteiro de Oliveira. No content or code of this web site may be reproduced without prior permission from the author.