Thrust Augmentation by Airframe-Integrated Linear-Spike Nozzle Concept for High-Speed Aircraft

The airframe-integrated linear-spike nozzle concept applied to an external nozzle for high-speed aircraft was evaluated with regard to the thrust augmentation capability and the trim balance. The main focus was on the vehicle aftbody. The baseline airframe geometry was first premised to be a hyperso...

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Bibliographic Details

Published in:	Aerospace
Main Authors:	Hidemi Takahashi, Toshihiko Munakata, Shigeru Sato
Format:	Article
Language:	English
Published:	MDPI AG 2018-02-01
Subjects:	supersonic/hypersonic transport linear aerospike nozzle airframe-propulsion integration aft-body external nozzle
Online Access:	http://www.mdpi.com/2226-4310/5/1/19