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MS: Recent submissions

Now showing items 21-30 of 30

FAILURE ANALYSIS OF HIGH-PRESSURE TURBINE BLADES OF A TURBOFAN ENGINE

Bhatti, Asad Mumtaz (CAE, NUST, 2023-06)

The turbine blades, which are exposed to a harsh environment, are one of the most important and vital components of a gas turbine. During each engine operating cycle, gas turbine blades are subjected to very high levels ...
DESIGN, ANALYSIS, AND PROTOTYPING OF VERTICAL AXIS WIND TURBINE FOR ENERGY HARVESTING

Muhammad Ahmad; Aamer Shahzad dr. (NUST CAE, 2021)

Among renewable energy sources, wind energy is considered an efficient, cost-effective, and accessible source of energy. Wind energy can be converted into electricity using wind turbines. This research aims to enhance the ...
STUDY OF CORROSION MECHANISMS ON HIGH PRESSURE TURBINE BLADE OF A TURBOFAN ENGINE

Sara Khushbash; Asad Hameed Dr. (NUST CAE, 2021)

A turbine blade is an advanced piece of technology and one of the vital and costly components in any modern aero-engine. They face extreme operating conditions of high stresses (~> 450 MPa), elevated temperatures (>1400 o ...
DESIGN, ANALYSIS, FLIGHT DYNAMICS MODELING, SIMULATION AND CONTROL OF VTOL HYBRID UNMANNED AERIAL VEHICLE

Muhammad Rehan; Farooq Bin Akram Dr (NUST CAE, 2021)
COMPUTATIONAL INVESTIGATION OF THE BYPASS DUAL THROAT FLUIDIC THRUST VECTORING NOZZLE

Saadia Afridi; Tariq Amin Khan Dr. (NUST CAE, 2021)

The thrust vector orientation is a proven idea for improving maneuverability, control efficiency, survivability, performance, and stealth characteristic of the aircraft. The thrust vector control system is gradually being ...
flight dynamics, control modeling and implementation of stability augmentation system for fixed wing micro air vehicle

Azhar Abbas; Nafees Mumtaz Qadri Dr (NUST CAE, 2021)
NUMERICAL ANALYSIS OF FLUID-STRUCTURE INTERACTION (FSI) OF FLAPPING WING FOR MAV APPLICATIONS

Syed Baleegh Hussain (NUST CAE, 2020)
COMPUTATIONAL INVESTIGATION AND FLOW FIELD ANALYSIS OF FLEXIBLE WING FOR HUMMINGBIRD-LIKE HOVERING MOTION

Naeem Haider; Aamer Shahzad Dr. (NUST CAE, 2021)

Flapping wing micro aerial vehicles are studied as the substitute for fixed and rotary wing micro aerial vehicles because of the advantages such as agility, maneuverability and employability in confined environments. ...
AERODYNAMIC DESIGN IMPROVEMENT OF HIGH-SPEED PROJECTILE

Ammar Hussain Farooqi; Mohtashim Mansoor Dr (NUST CAE, 2021)

Projectiles with efficient aerodynamics and advanced guidance technology are now the need for modern military inventory. The multifaceted approach to technology has led to the development of advanced projectiles having ...
DESIGN AND DEVELOPMENT OF AERIAL PLATFORMS FOR INTELLIGENT FLIGHT IN SWARM CONFIGURATION

Muhammad Sohaib Khan; Syed Irtiza Ali Shah Dr. (NUST CAE, 2021)

In this study, different multirotor UAV configurations have been studied for the selection of the best configuration for a small but heavy-lift multirotor. The coaxial/overlapping configurations have been found to increase ...

Now showing items 21-30 of 30

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