高马赫数超燃冲压发动机技术研究进展

岳连捷, 张旭, 张启帆, 陈科挺, 李进平, 陈昊, 姚卫… - 力学学报, 2022 - lxxb.cstam.org.cn
吸气式高超声速飞行在空间运输和国家空天安全领域具有极高价值, 超燃冲压发动机是其核心
动力装置. 目前飞行马赫数4.0~ 7.0 超燃冲压发动机技术日趋成熟, 发展更高速的飞行动力技术 …

Research progress on high-Mach-number scramjet engine technologies

Y Lianjie, Z Xu, Z Qifan, C Keting… - Chinese Journal of …, 2022 - lxxb.cstam.org.cn
Hypersonic airbreathing flights are highly valued in both the fields of space transportation
and national aerospace safety, and the scramjet engines are pivotal propulsion devices for …

Rugged, scramjet inlet temperature and velocity sensor: design and ground test

J Kurtz, M Aizengendler, Y Krishna, P Walsh, S O'Byrne - AIAA Journal, 2016 - arc.aiaa.org
The design and testing of a gas temperature and velocity scramjet engine inlet sensor based
on tunable diode laser absorption spectroscopy of oxygen is discussed. The robustness and …

Patterns of steady axisymmetric supersonic compression flows with a Mach disk

YP Gounko - Shock Waves, 2017 - Springer
Results of a numerical simulation of steady axisymmetric supersonic flows in convergent
conical ducts and in overexpanded jets are presented. The characteristic feature of these …

Modal Analysis of a Scramjet Inlet for Optimization of Sensor Placement

L Pollock, G Wild - ASCEND 2021, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-4084. vid Hypersonic vehicles,
generally defined as those that operate great than Mach 5 and in which aerodynamic …

Investigating endo-atmospheric separation of a hypersonic flyer-sustainer using wind tunnel based free-flight

LP McQuellin, CM Kennell, JM Sytsma… - 23rd AIAA international …, 2020 - arc.aiaa.org
While atmospheric flight-testing is the only indisputable way to demonstrate the technical
feasibility of a flight-vehicle design, the risks of this relatively expensive exercise are …

Considerations for a hypersonic flight test investigating fluid-thermal-structural interactions

LP McQuellin, A Neely, G Currao - 23rd AIAA International Space …, 2020 - arc.aiaa.org
Sustained hypersonic flight remains a state-of-the-art problem, with limited examples of
vehicles capable of performing in this extreme environment for extended periods of time …

Numerical modeling of the conditions for realization of flow regimes in supersonic axisymmetric conical inlets of internal compression

YP Gounko, II Mazhul - Thermophysics and Aeromechanics, 2015 - Springer
The results of the numerical investigation of flow regimes in the axisymmetric inlets of
internal compression at a supersonic flow around them are presented in the work. The main …

Subsonic in-flight temperature and pressure measurements using a scramjet inlet flow sensor

J Kurtz, M Aizengendler, Y Krishna, P Walsh, M Brown… - Aiaa Journal, 2016 - arc.aiaa.org
The performance of a scramjet inlet sensor based on tunable diode laser absorption
spectroscopy of oxygen in the A-band near 760 nm during a low-altitude, subsonic flight test …

A Historical Review Sounding Rockets and their use in Hypersonics Research

DJ McDonell, KK Ahuja - AIAA SCITECH 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0769. vid This paper provides a
state-of-the-art review of the research conducted using sounding rockets with particular …