Results 51 to 60 of about 2,515 (186)

Study of an adaptive bump control mechanism for shock wave/boundary layer interactions in supersonic flows

open access: yesTheoretical and Applied Mechanics Letters
The stability of supersonic inlets faces challenges due to various changes in flight conditions, and flow control methods that address shock wave/boundary layer interactions under only one set of conditions cannot meet developmental requirements.
Shan-Shan Tian   +4 more
doaj   +1 more source

Analysis of Air-Breathing Hypersonic Maneuver Flight Styles and Key Technologies [PDF]

open access: yesHangkong bingqi
The maneuver flight performance is one of the key capabilities to ensure the implementation of various applications for air-breathing hypersonic aircraft.
Duan Pengfei, Gao Shuliang, Wang Enliang, Wang Han
doaj   +1 more source

The Unintended Consequences of German Deterrence

open access: yesGlobal Policy, EarlyView.
ABSTRACT Germany's evolving deterrence posture boils down to continued participation in NATO nuclear sharing and an ambitious conventional rearmament program. Due to its non‐nuclear status and a result of decades of underinvestment, Germany prioritizes modern conventional weapons.
Ulrich Kühn
wiley   +1 more source

Influence of Incident Shock on Fuel Mixing in Scramjet

open access: yesApplied Sciences
During the operation of hypersonic vehicles, a reciprocal coupling effect is manifested between the inlet and the combustion chamber. This results in an unavoidable non-uniformity of conditions at the combustion chamber’s entrance, which, in turn ...
Chao Wang   +3 more
doaj   +1 more source

Universities as the Next Counterintelligence Battleground in Geopolitical Contests

open access: yesGlobal Policy, EarlyView.
ABSTRACT Globally, universities are increasingly becoming the target of foreign national security actors, engaging in espionage, sabotage, foreign interference and intellectual property theft. Despite that, there has been no examination of the utilisation of counterintelligence approaches by universities to the threats they face from the subordination ...
Brendan Walker‐Munro   +1 more
wiley   +1 more source

Advances in Research on High-Mach-Number Electromagnetic Flow Control Effectiveness

open access: yes气体物理
The electromagnetic flow control technology under high-altitude and high-speed flight conditions can be applied in multiple fields such as thermal protection, separation zone control, alleviating ionization blackout problems, aerodynamic shape design ...
Yang DU, Jun LIU
doaj   +1 more source

Risk Scenarios for European Rearmament

open access: yesGlobal Policy, EarlyView.
ABSTRACT Since Russia's invasion of Ukraine in 2022, the European Union has launched a flurry of initiatives to ramp up European defence spending. Efforts to bolster European defence have further intensified in response to the United States' increasingly hostile stance towards its erstwhile European allies.
Mette Eilstrup‐Sangiovanni
wiley   +1 more source

Parametric analysis of aerodynamic-propulsion integratedperformance for hypersonic vehicles

open access: yesKongqi donglixue xuebao
To parametrically assess the aerodynamic-propulsion integrated performance of air-breathing hypersonic vehicles and comprehensively elucidate the influence rules of overall vehicle parameters on their performance, this paper proposes a parametric ...
Jingfan Chen, Xiaoqiang Fan, Bing Xiong
doaj   +1 more source

The Continuity and Rupture of the ‘New Washington Consensus’: From Biden to Trump 2.0

open access: yesGlobal Policy, EarlyView.
ABSTRACT The ‘New Washington Consensus’ (NWC) represents a major intellectual shift in the US approach to global economic governance. However, the NWC has never been subject to systematic academic critique. With Trump's return to the White House ushering in a new era of US trade policy, the NWC is widely considered to be politically irrelevant in the ...
Ming Du
wiley   +1 more source

An Analysis of the Factors Influencing Dual Separation Zones on a Plate

open access: yesApplied Sciences
The shock wave/boundary layer interaction phenomenon in hypersonic inlets, affected by background waves, may induce the formation of multiple separation zones.
Jiarui Zou, Xiaoqiang Fan, Bing Xiong
doaj   +1 more source

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