Aerodynamic Instabilities in High-Speed Air Intakes and Their Role in Propulsion System Integration
AL Philippou, PK Zachos, DG MacManus - Aerospace, 2024 - mdpi.com
High-speed air intakes often exhibit intricate flow patterns, with a specific type of flow
instability known as 'buzz', characterized by unsteady shock oscillations at the inlet. This …
instability known as 'buzz', characterized by unsteady shock oscillations at the inlet. This …
Comparison of the unstart/restart processes of a two-dimensional twin-duct supersonic inlet induced by the plug throttling and thermal choking at the sideslip state
T Li, R Ding, W Wang, W Xie - Aerospace Science and Technology, 2023 - Elsevier
It is of great significance to study the hysteresis phenomenon in the unstart/restart process of
supersonic inlets for restart control in the practical operation of ramjet engines. In this paper …
supersonic inlets for restart control in the practical operation of ramjet engines. In this paper …
Flowfield characteristics in sidewall compression inlets
G Xiang, X Gao, X Jie, X Li, H Li, X Chen - Acta Mechanica Sinica, 2020 - Springer
In this work, the flow fields in three-dimensional (3D) sidewall compression inlets are
investigated theoretically and numerically. Combining spatial dimension reduction theory …
investigated theoretically and numerically. Combining spatial dimension reduction theory …
Investigating the legacy of air-breathing and rocket propulsion systems
JP Jones, L Kuffel, E Sorto-Ramos… - AIAA Propulsion and …, 2020 - arc.aiaa.org
Resurgence of interest in hypersonic and space-access vehicles increases the demand for
an educated workforce. A valuable approach to immediately educate a new generation of …
an educated workforce. A valuable approach to immediately educate a new generation of …
Exploration of optimal propulsion system airframe integration design concepts for a low boom supersonic aircraft
View Video Presentation: https://doi. org/10.2514/6.2021-2469. vid We consider several
approaches on propulsion system airframe integration design concepts for supersonic …
approaches on propulsion system airframe integration design concepts for supersonic …
[PDF][PDF] ISTANBUL TECHNICAL UNIVERSITY 击GRADUATE SCHOOL
R IMRAK - 2023 - polen.itu.edu.tr
ISTANBUL TECHNICAL UNIVERSITY 击GRADUATE SCHOOL PROPULSION-AIRFRAME
INTEGRATION FOR LOW-BOOM SUPERSONIC AIRCRAFT M.Sc. THESIS Page 1 ISTANBUL …
INTEGRATION FOR LOW-BOOM SUPERSONIC AIRCRAFT M.Sc. THESIS Page 1 ISTANBUL …
[PDF][PDF] Passive Flow Modification Over the Supersonic and the Hypersonic Air-Intake System Using Bleed.
The air intake should be operated at design conditions to achieve a high total pressure
recovery and optimum mass capture ratio. The current research focuses on the numerical …
recovery and optimum mass capture ratio. The current research focuses on the numerical …
Accelerative Starting of Busemann Air Intakes
S Suman - 2024 - escholarship.mcgill.ca
The flow-starting requirements play a crucial role in the design of air intakes. It may be
challenging to achieve flow-starting in high-contraction ratio intakes using the quasi-steady …
challenging to achieve flow-starting in high-contraction ratio intakes using the quasi-steady …
Numerical Study of Shock-Dominated Flow Control in Supersonic Inlets
DE Wagner - 2023 - search.proquest.com
This thesis concentrates on the improvement of the quality of shock-dominated flows in
supersonic inlets by controlling shock wave/boundary layer interactions (SWBLIs). SWBLI …
supersonic inlets by controlling shock wave/boundary layer interactions (SWBLIs). SWBLI …
[PDF][PDF] ISTANBUL TECHNICAL UNIVERSITY★ GRADUATE SCHOOL
B ÇETİN - 2023 - polen.itu.edu.tr
(McFarland and Gomez, 2016). Organizations have become so ubiquitous that they have
become the medium of modern social life; we can't picture existence without them. Many of …
become the medium of modern social life; we can't picture existence without them. Many of …