Development of Constant Rate of Momentum Change | Based Variable Area Nozzle

Ankit Sharma (u. a.)

ISBN 10: 6207462807 / ISBN 13: 9786207462803

Published by LAP LAMBERT Academic Publishing, 2024

About this Item

Development of Constant Rate of Momentum Change | Based Variable Area Nozzle | Ankit Sharma (u. a.) | Taschenbuch | Englisch | 2024 | LAP LAMBERT Academic Publishing | EAN 9786207462803 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu.

Seller Inventory # 128645025

Bibliographic Details

• Title: Development of Constant Rate of Momentum Change | Based Variable Area Nozzle
• Publisher: LAP LAMBERT Academic Publishing
• Publication Date: 2024
• Language: English
• ISBN 10: 6207462807
• ISBN 13: 9786207462803
• Binding: Taschenbuch
• Condition: Neu
• Dimensions: 220W x 150H x 4D millimeters 220 millimeters width by 150 millimeters height by 4 millimeters depth
• Weight: 96 grams
• Seller catalogs:
  • Bücher

About this title

Synopsis

A nozzle is a mechanical device which is designed to control the rate of flow, speed, direction, and pressure of the stream that exhaust through it. There are various types of nozzles which are used. In a nozzle, the velocity of fluid increases at the expense of its pressure energy. Nozzle specifically is a device which is developed and designed to control the direction of the fluid flowing in any motion, the nozzle's primary role is to control the characteristics of fluid flow, just like to increase the velocity as it exits the chamber of a propulsive system. In the thesis the Computational Fluid Dynamic (CFD) analysis to study on supersonic variable area nozzle with frictional effects. The investigation is to find the ways to improve the performance of nozzle systems. This is mainly concentrated on the design and analysis of CRMC nozzle with frictional effect. The results are shown based on contour and graphical. A graph represents acc. to analytical and CFD. As observed from results, that Mach number is increasing with increasing axial distance along CRMC nozzle.