WorldofAerospace.googlepages.com                                                            Contact Us | Sitemap | Home
 

 Calculate Temperature at Stagnation Point of Blunt Nose Body

 Method to Calculate the Temperature at Stagnation Point at the Nose of the Body

 

Aerospace

 

 Aerospace

 Aerospace Engineering

 Aeronautical Engineering

 Aeronautics

 Astronautics

 Space Exploration

 Aerospace Industry

 Aerospace Related Questions

 Aerospace Related Articles

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

How to Calculate the Temperature at the Stagnation Point of a Blunt Shaped Body

In this article, we would look into how can we calculate the temperature at the stagnation point at the nose of the body. For this purpose, we have considered a blunt shaped body. 

 

 

For this purpose, we have considered that the Blunt shaped body is placed in the test section of a supersonic wind tunnel.

 

We Require,

The Reservoir Pressure in atm and

The Reservoir Temperature in degree Rankine

Furthermore, we require the Mach no. of the flow in the test section.

 

Performing the calculation, gives us the Exit pressure Pe and the Stagnation Temperature at the nose of the body given by Tstag which has units of degree Rankine.

 

Download Free Program to Calculate the Temperature at the Stagnation Point