Computational study on chamber morphing wing concept for efficient lift at various angle of attack
Bilji c Mathew ; K. Sai Priyanka ; J V Muruga Lal Jeyan All Authors
Articles
Design and analysis for the flutter behaviour of different selected wing plan forms computationally
Abstract: The objective behind this work is to analyse different aerofoils and study their flutter behaviour and the trying to understand the influence the aerofoil parameters has on the dynamic aero-elastic behaviour of the wing that is constructed by that aerofoil. In an attempt to understand this, wings of same span and chord dimensions are
Albatross and F oss and Falcon inspir alcon inspired Bionic U ed Bionic UAV: An Aer V: An Aerodynamic odynamic Analysis
Bilji C. Mathew Lovely Professional University, [email protected] Sagar K. Sahu Lovely Professional University, [email protected] Prantik Dutta Lovely Professional University, [email protected] Rushi Savale Lovely professional university, [email protected] Muruga Lal Jeyan JV Dr. Lovely professional University, [email protected]
Evolutionary and Hereditary Traits of an Albatross and its Aerodynamic Optimality
To cite this article: Bilji C Mathew et al 2021 IOP Conf. Ser.: Earth Environ. Sci. 775 012002
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Computational study for improvement of aerodynamic performance of airfoil by changing various aerodynamic properties
Abstract An airfoil is a cross-section of a wing that is normal to the span of the wing. Generally, we called it a two-dimensional view of the wing and play important role in the preliminary design of an aircraft. The selection of an airfoil is primarily based on various parameter such as thickness maintenance for
Effect of camber on the flutter characteristics of different selected airfoils
R. Sabari VIHAR*,1 , J. V. Muruga Lal JEYAN1 , K. Sai PRIYANKA1 *Corresponding author 1 Department of Aeronautical Engineering, Lovely Professional University, Punjab, [email protected]*, [email protected], [email protected] DOI: 10.13111/2066-8201.2021.13.3.18 Received: 07 June 2021/ Accepted: 31 July 2021/ Published: September 2021 Copyright © 2021. Published by INCAS. This is an “open acccess” article
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Comparative study on per e study on performance accur formance accuracy of thr acy of three probe and obe and five probe flow analysers for wind tunnel testing
Akhila Rupesh Ms Lovely Professional University, [email protected] J V Muruga Lal Jeyan Dr Lovely Professional University, [email protected]
Evaluation of design criteria for mini unmanned aircraft systems (UAS) applications
Abstract Purpose – This paper aims to evaluate the factors that dictate the design of a mini unmanned aircraft system (UAS). Design/methodology/approach – This paper analyses various dimensions that dictate the design criteria for a mini UAS. Findings – Compared to civil applications, design of mini UAS for military application is much more challenging owing
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Comparative Analysis of Fixed-Wing, Rotary-Wing and Hybrid Mini Unmanned Aircraft Systems (UAS) from the Applications Perspective
Abstract: Mini Unmanned Aircraft Systems (UAS) present distinct design challenges due to their manportable, field-deployable profile. The implications of various unmanned aerial vehicle (UAV) design configurations for Mini UAS applications are discussed in this study. Fixed-wing, rotary-wing, and hybrid Mini UAS design configurations are analysed and compared based on performance parameters specified by various manufacturers
The Influence of Social Customer Relationship Management on Brand Loyalty : Case of Thailand’s Luxury Hotel
A Thesis Submitted in Partial Fulfilment of the Requirements for Degree of Doctor of Business Administration (Hospitality Management) Programme Validated & Certified by European International University – Paris This thesis is approved for recommendation to the European International University, Paris, by Asia eLearning Management Center, Singapore. Examination Committee: Asst. Prof. Dr Wasutida Nurittamont (Advisor) Dr