Estimation of the virtual masses of a large unconventional airship based on purely analytical method to aid in the preliminary design
- 1 September 2021
- journal article
- research article
- Published by Emerald in Aircraft Engineering and Aerospace Technology
- Vol. 94 (4), 531-540
- https://doi.org/10.1108/aeat-12-2020-0304
Abstract
This paper presents preliminary results of the modeling of a large autonomous quad-rotor airship, with flying wing shape. This airship is supposed to be a flexible body. This study promotes an entirely analytical methodology with some assumptions. In this study and as first assumption, the shape of the careen is supposed to be an elliptic cone. To retrieve the velocity potential shapes, this paper solved the Laplace’s equation by using the sphero-conal coordinates. This leads to the Lamé’s equations. The whole system equations governing the interaction of air–structure, including the boundary conditions, is solved in an analytical setting. This paper opted for a modeling and determination of the added masses of a flexible airship by an analytical method illustrated by a comparison with a geometric method. This analytical method includes the study of complex functions which are the Lamé functions. This paper provides an analytical way to estimate an aerodynamic phenomenon which acts on the airship and in particular on its envelope and known as the phenomenon of added masses or virtual masses, as well as the means of defining it and the calculation analytically for the case of the flexible airship. Considering that the calculation of the added masses is very difficult and the numerical methods increase the number of degrees of freedom, the analytical method established in this paper has become a solution of calculations of these virtual masses. This paper includes an application for determining the added masses of a new generation MC500 airship. This paper allows defining an analytical method which determines the added masses of an airship, which helps the automation engineer to develop a control strategy to stabilize this airship.Keywords
This publication has 14 references indexed in Scilit:
- Visualization of vortex flow field around a flat plate with noncircular holeIOP Conference Series: Materials Science and Engineering, 2018
- Heuristic optimization of Bezier curves based trajectories for unconventional airships dockingAircraft Engineering and Aerospace Technology, 2017
- Airship dynamics modeling: A literature reviewProgress in Aerospace Sciences, 2011
- Contribution of the added masses in the dynamic modelling of flexible airshipsNonlinear Dynamics, 2011
- A review of airship structural research and developmentProgress in Aerospace Sciences, 2009
- Dynamics Modeling and Simulation of Flexible AirshipsAIAA Journal, 2009
- Modelling and Control of Flexible AirshipAIP Conference Proceedings, 2008
- Nonlinear airship aeroelasticityJournal of Fluids and Structures, 2005
- The Autonomous Blimp Project of LAAS-CNRS: Achievements in Flight Control and Terrain MappingThe International Journal of Robotics Research, 2004
- THE COMPLETE EXPRESSIONS FOR ADDED MASS OF A RIGID BODY MOVING IN AN IDEAL FLUIDPublished by Defense Technical Information Center (DTIC) ,1961