Share
Design of CRMC Non-Adiabatic Supersonic Nozzle
Virendra Kumar
(Author)
·
Surendra Kumar Yadav
(Author)
·
Shambhu Pandit
(Author)
·
LAP Lambert Academic Publishing
· Paperback
Design of CRMC Non-Adiabatic Supersonic Nozzle - Pandit, Shambhu ; Kumar, Virendra ; Yadav, Surendra Kumar
Choose the list to add your product or create one New List
✓ Product added successfully to the Wishlist.
Go to My Wishlists
Origin: U.S.A.
(Import costs included in the price)
It will be shipped from our warehouse between
Friday, July 26 and
Friday, August 02.
You will receive it anywhere in United Kingdom between 1 and 3 business days after shipment.
Synopsis "Design of CRMC Non-Adiabatic Supersonic Nozzle"
In engineering systems like jet propulsion, steam turbines, gas turbines, and jet engines, nozzles are crucial parts. They increase the speed of fluid flow from subsonic to supersonic or hypersonic levels, producing the required thrust under certain design and operating circumstances. The efficiency, thrust, and flow rate of the nozzle are determined by its shape and flow characteristics, making its design and analysis essential to the optimization of a variety of engineering systems. In this work, sophisticated propelling nozzles are designed and analysed, with an emphasis on their form and flow characteristics. Nozzle length is taken into account, along with the assumption of constant momentum rate, and 1-D gas dynamic equations are used to examine these variables.The constant rate of momentum change (CRMC) hypothesis, which incorporates frictional effects and heat addition, is utilised to obtain consistent flow characteristics at any distance. The findings of the CRMC theory are validated using computational fluid dynamics (CFD) using ANSYS Workbench 2022R2, which reveals that under design conditions, the numerical conclusions and the CRMC theory results are in agreement.