The present work deals with a detailed parametric thermodynamic analysis of all the possible configurtions of a turbofan engine (two and three spool with or without13; mixer and/ afterburner). The study focuses on design point performance and is of general nature rather than an application specific parametric study. The analysis13; has been carried out by selecting/developing models for various components of engine. A set of multi-dimensional carpet plots predicting the effect of dependent in13; terms of independent parameters has been presented considering transpiration coolingtechnique for turbine blades and the temperature effect on specific heat of13; air/gas. Besides giving the comparative design point performance for a class of turbof...
An inter turbine combustion is one of modern direction of turbofan engine cycle modification. It is ...
Presented herein is a comparative performance analysis of a novel turbofan engine with an auxiliary ...
This research introduces the reader to a brief analysis of various types of aircraft engines, with p...
The present work deals with a detailed parametric thermodynamic analysis of all the possible configu...
The present work deals with a detailed parametric thermodynamic analysis of all the possible configu...
The present work deals with a detailed parametric thermodynamic analysis of all the possible configu...
The turbofan engines are widely used as propulsion of the contemporary airplanes. In the military ap...
This study focuses on the parametric cycle analysis of a dual-spool, separate-flow turbofan engine w...
ABSTRACT In this paper Turbofan engine performance graphs including thrust, thrust specific fuel con...
An account is given of mixed flow turbofan engine performance calculation results for the design poi...
An account is given of mixed flow turbofan engine performance calculation results for the design poi...
The problems of turbofan engines development is briefly discussed in the beginning. Next the concept...
Implementation of Variable Geometry during the off-design operation of an aero gas turbine engine m...
The purpose of this paper is to set up a method to determine the missing engine design parameters (t...
During the forthcoming years many new aircrafts such as A350 and B787 are being designed and continu...
An inter turbine combustion is one of modern direction of turbofan engine cycle modification. It is ...
Presented herein is a comparative performance analysis of a novel turbofan engine with an auxiliary ...
This research introduces the reader to a brief analysis of various types of aircraft engines, with p...
The present work deals with a detailed parametric thermodynamic analysis of all the possible configu...
The present work deals with a detailed parametric thermodynamic analysis of all the possible configu...
The present work deals with a detailed parametric thermodynamic analysis of all the possible configu...
The turbofan engines are widely used as propulsion of the contemporary airplanes. In the military ap...
This study focuses on the parametric cycle analysis of a dual-spool, separate-flow turbofan engine w...
ABSTRACT In this paper Turbofan engine performance graphs including thrust, thrust specific fuel con...
An account is given of mixed flow turbofan engine performance calculation results for the design poi...
An account is given of mixed flow turbofan engine performance calculation results for the design poi...
The problems of turbofan engines development is briefly discussed in the beginning. Next the concept...
Implementation of Variable Geometry during the off-design operation of an aero gas turbine engine m...
The purpose of this paper is to set up a method to determine the missing engine design parameters (t...
During the forthcoming years many new aircrafts such as A350 and B787 are being designed and continu...
An inter turbine combustion is one of modern direction of turbofan engine cycle modification. It is ...
Presented herein is a comparative performance analysis of a novel turbofan engine with an auxiliary ...
This research introduces the reader to a brief analysis of various types of aircraft engines, with p...