An aerolance system

University of Southern Queensland (2014) An aerolance system. .

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Abstract

An aerolance system for an aerospace vehicle including a head for positioning adjacent a nose of the aerospace vehicle. The head includes a divergent section and a convergent section wherein a base of the convergent section is positioned adjacent a base of the divergent section, and wherein the head includes a cavity for ejecting fluid out of the head.


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Item Type: Patent
Item Status: Live Archive
Additional Information: WO2014008549 (A1)
Faculty/School / Institute/Centre: Current - Faculty of Health, Engineering and Sciences - School of Mechanical and Electrical Engineering (1 Jul 2013 -)
Faculty/School / Institute/Centre: Current - Faculty of Health, Engineering and Sciences - School of Mechanical and Electrical Engineering (1 Jul 2013 -)
Date Deposited: 28 Sep 2016 23:43
Last Modified: 07 Sep 2021 03:19
Uncontrolled Keywords: aeronautics; increasing speed; speed of sound; fuel efficiency; drag load; heating load
Fields of Research (2008): 09 Engineering > 0901 Aerospace Engineering > 090108 Satellite, Space Vehicle and Missile Design and Testing
09 Engineering > 0915 Interdisciplinary Engineering > 091505 Heat and Mass Transfer Operations
09 Engineering > 0901 Aerospace Engineering > 090107 Hypersonic Propulsion and Hypersonic Aerodynamics
Fields of Research (2020): 40 ENGINEERING > 4001 Aerospace engineering > 400107 Satellite, space vehicle and missile design and testing
40 ENGINEERING > 4012 Fluid mechanics and thermal engineering > 401205 Experimental methods in fluid flow, heat and mass transfer
40 ENGINEERING > 4001 Aerospace engineering > 400106 Hypersonic propulsion and hypersonic aerothermodynamics
Socio-Economic Objectives (2008): E Expanding Knowledge > 97 Expanding Knowledge > 970109 Expanding Knowledge in Engineering
URI: http://eprints.usq.edu.au/id/eprint/26962

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