Investigation of translation scheme turbine-based combined-cycle inlet mode transition
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference20 articles.
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2. Experimental and numerical investigations on the mode transition process of an exhaust system for an over-under turbine based combined cycle;Lv;Aerosp. Sci. Technol.,2020
3. Trajectory optimization for a TBCC-powered supersonic vehicle with transition thrust pinch;Zheng;Aerosp. Sci. Technol.,2019
4. Conceptual design of a two-stage-to-orbit vehicle using SABRE engines;Brevault,2019
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