Výsledky vyhledávání - "Raees Fida Swati"

Akademický článek

Development of a Predictive Tool for the Parametric Analysis of a Turbofan Engine

Autor: Zara Ahmed, Muhammad Umer Sohail, Asma Javed, Raees Fida Swati

Publikováno v: Applied Sciences, Vol 13, Iss 19, p 10761 (2023)

Parametric cycle analysis, an on-design engine study, specifies the required design characteristics that optimize engine performance. This study aimed to conduct a parametric analysis of a low-bypass turbofan engine with an afterburner, F100-PW229, a

Externí odkaz: https://doaj.org/article/9c4d8a9b524542f58dab30576b5bd543

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Akademický článek

Flow Boiling of Liquid n-Heptane in Microtube with Various Fuel Flow Rate: Experimental and Numerical Study

Autor: Muhammad Tahir Rashid, Naseem Ahmad, Raees Fida Swati, Muhammad Bilal Khan

Publikováno v: Micromachines, Vol 14, Iss 9, p 1760 (2023)

The evaporation of liquid hydrocarbon n-heptane is discussed in detail with experimentation and numerical techniques. A maximum wall temperature of 1050 K was reported during an experimental process with a two-phase flow that was stable and had a pro

Externí odkaz: https://doaj.org/article/65f23c0693c4461fb02089ea9801c1b5

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Akademický článek

Comparison of Optimization Techniques and Objective Functions Using Gas Generator and Staged Combustion LPRE Cycles

Autor: Suniya Sadullah Khan, Ihtzaz Qamar, Muhammad Umer Sohail, Raees Fida Swati, Muhammad Azeem Ahmad, Saad Riffat Qureshi

Publikováno v: Applied Sciences, Vol 12, Iss 20, p 10462 (2022)

This paper compares various optimization techniques and objective functions to obtain optimum rocket engine performances. This research proposes a modular optimization framework that provides an optimum design for Gas Generator (GG) and Staged Combus

Externí odkaz: https://doaj.org/article/805955c91d66450e97effb73c40a84fb

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Akademický článek

Effect of Secondary Combustion on Thrust Regulation of Gas Generator Cycle Rocket Engine

Autor: Sohaib Khan, Muhammad Umer Sohail, Ihtzaz Qamar, Muzna Tariq, Raees Fida Swati

Publikováno v: Applied Sciences, Vol 12, Iss 20, p 10563 (2022)

Thrust regulation is applied to maintain the performance of the liquid propellant rocket engine. The thrust level of a rocket engine can be readily controlled by adjusting the number of propellants introduced into the combustion chamber. In this stud

Externí odkaz: https://doaj.org/article/c6d2b009254246d693c42f99bf8e04a0

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Akademický článek

Micro-Mechanical Investigation of Interfacial Debonding in Carbon Fiber-Reinforced Composites Using Extended Finite Element Method (XFEM) Approach

Autor: Raees Fida Swati, Saad Riffat Qureshi, Muhammad Umer Sohail, Adnan Munir, Omer Masood Qureshi, Abid Ali Khan

Publikováno v: Micromachines, Vol 13, Iss 8, p 1226 (2022)

The interface debonding in carbon fiber-reinforced polymers is analyzed and evaluated using the extended finite element method (XFEM). In order to accurately evaluate the bonding properties between fibers and matrix, different tests were carried out,

Externí odkaz: https://doaj.org/article/1216cd22812746dc8b80f5d92b313de0

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