Flow Pattern In A Converging-diverging Nozzle

by Nasa Technical Reports Server (ntrs)

2021-01-26 18:13:47

The present report describes a new method for the prediction of the flow pattern of a gas in the two-dimensional and axially symmetrical case. It is assumed that the expansion of the gas is adiabatic and the flow stationary. The several assumptions n... Read more
The present report describes a new method for the prediction of the flow pattern of a gas in the two-dimensional and axially symmetrical case. It is assumed that the expansion of the gas is adiabatic and the flow stationary. The several assumptions necessary of the nozzle shape effect, in general, no essential limitation on the conventional nozzles. The method is applicable throughout the entire speed range; the velocity of sound itself plays no singular part. The principal weight is placed on the treatment of the flow near the throat of a converging-diverging nozzle. For slender nozzles formulas are derived for the calculation of the velocity components as function of the location. Less

Book Details

ISBN9781289104917

Compare Prices

Store Availability Book Format Condition Price
Indigo Books & Music In Stock Buy CAD 18.99
Indigo Books & MusicIn Stock
Format
Condition
Buy CAD 18.99
Available Discount
No Discount available

Join us and get access to all
your favourite books

Sign up for free and start exploring thousands of eBooks today.

Sign up for free