Buoyancy Lift AugmentationYuvaraj G* and Veeranjaneyulu K
Department of Aeronautical Engineering, Marri Laxman Reddy Institute of Technology, Laxman Reddy Avenue, Dundigal 500043, Hyderabad
- *Corresponding Author:
- Yuvaraj G
Department of Aeronautical Engineering
Marri Laxman Reddy Institute of Technology
Laxman Reddy Avenue, Dundigal 500043, Hyderabad
E-mail: [email protected]
Received Date: July 27, 2016; Accepted Date: October 26, 2016; Published Date: October 31, 2016
Citation: Yuvaraj G, Veeranjaneyulu K (2016) Buoyancy Lift Augmentation. J Aeronaut Aerospace Eng 5:175. doi: 10.4172/2168-9792.1000175
Copyright: © 2016 Yuvaraj G, et al. This is an open-access article distributed under the terms of the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credited.
This paper proposes an idea of lift augmentation for conventional subsonic aircraft at low along with mathematical analysis. This paper mainly addresses certain changes in power plant requirements and performance characteristics of aircraft after implementation of buoyancy lift augmentation technique. There are certain factors which must be considered for practical implementation of it towards an aircraft without degrading its primary performance and mission profile. Those considerations are discussed with respect to total weight or overall weight of the aircraft and vital changes required in design, manufacturing and operation are addressed. This document also formulates a brief overview on changes that would occur in flight aerodynamic characteristics after the supplementation as well as its impact on flight performance parameters.