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293 articles
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Aerodynamics and flow pattern performance evaluation of off road vehicle for various velocity range and angle of incidence
To cite this article: JV Muruga Lal Jeyan et al 2020 J. Phys.: Conf. Ser. 1473 012001
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Effects of secondary injection on the performance of over-expanded single expansion ramp nozzle
To cite this article: Gopinath Shanmugaraj et al 2020 J. Phys.: Conf. Ser. 1473 012002
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A review on Aerodynamic performance of NACA Airfoil for various Reynolds number
To cite this article: Bilji C Mathew et al 2020 J. Phys.: Conf. Ser. 1473 012003
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Review on influence of radiating and aerodynamic shock at hypersonic vehicle
To cite this article: R Balaji et al 2020 J. Phys.: Conf. Ser. 1473 012004
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AC Loss Analysis on Coated Conductors at different Sinusoidal Frequencies for Electric Propulsion Applications
To cite this article: Abhinav Kumar et al 2020 IOP Conf. Ser.: Mater. Sci. Eng. 756 012027
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A Review on a Reassess Swot up on Airfoil Stall and Flow Separation Delay for a Range of Limitations Associated with Aerodynamics and Wing Profile.
K.Sai Priyanka 1 , J V Muruga Lal Jeyan*2 , R.Sabari Vihar3 1 Research scholar Lovely Professional University *2 Lovely Professional University 3 Institute of Aeronautical Engineering 1 [email protected], 2* [email protected], 3 [email protected]
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Mini Unmanned Aerial Systems (UAV) – A Review of the Parameters for Classification of a Mini U ameters for Classification of a Mini UAV.
Ramesh PS Lovely Professional University, [email protected] Muruga Lal Jeyan Lovely professional university, [email protected]
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Experimental and Computational Evaluation of Five Hole Five Probe Flow Analyzer for Subsonic Wind Calibration
Akhila Rupesh Ms Lovely Professional University, [email protected] J V Muruga Lal Jeyan Dr Lovely Professional University, [email protected]
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Terrain imperatives for Mini unmanned aircraft systems applications
P.S. Ramesh and J.V. Muruga Lal Jeyan Department of Aerospace, School of Mechanical Engineering, Lovely Professional University, Phagwara, India
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Performance analysis on varies bluff bodies at hypersonic speed
R Balaji ; Muruga Lal Jeyan All Authors
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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
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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…
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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,…
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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…
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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…
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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]
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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…
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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…
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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…