Results 11 to 20 of about 166,033,218 (291)

Secondary Acute Angle-Closure Attack: Diagnosis and Management [PDF]

open access: yesSiriraj Medical Journal, 2018
Patients may come with acute angle-closure attack that mimics primary disease, but actually there was a hidden cause. Mostly, fellow eye with wide open angle might be a clue for secondary cause. However, an area with high prevalence of narrow angle makes
Sakaorat Petchyim
doaj   +4 more sources

Design of Three-Dimensional Vector Guidance Law for Attack Time and Angle under Field of View Angle Constraints [PDF]

open access: yesHangkong bingqi
In order to enhance the precision of missile strikes on targets, controlling the three-dimensional gui-dance problem involving attack time and attack angle is of significant importance in practical applications.
Xiong Tianhao, Wang Changyuan, Zhang Ke, Su Yu, Guo Zhengyu
doaj   +2 more sources

Research on Aircraft Attack Angle Control Considering Servo-Loop Dynamics [PDF]

open access: yesInternational Journal of Aerospace Engineering, 2015
This paper presents a novel robust attack angle control approach, which can effectively suppress the impacts from system uncertainties and servo-loop dynamics.
Xiaodong Liu   +3 more
doaj   +2 more sources

Some experimental and theoretical studies in aircraft stability at high angles of attack [PDF]

open access: yes, 1983
A review of techniques for stability and response investigations is presented and the averaging technique of Beecham- Titchener-Simpson is applied to the lateral equations of. motion for two combat aircraft.
Thorne, R.
core   +7 more sources

Influence of attack angle on ventilated supercavitating flow at high Froude number condition

open access: yesXibei Gongye Daxue Xuebao, 2022
To study the influence of attack angle on ventilated supercavitating flow, a numerical model is established to simulate the supercavitation flow by using the inhomogeneous multiphase flow model and the SST k-ω turbulence model.
WANG Yifei   +4 more
doaj   +1 more source

Research on Sailing Efficiency of Hybrid-Driven Underwater Glider at Zero Angle of Attack

open access: yesJournal of Marine Science and Engineering, 2021
The sailing efficiency of an underwater glider, an important type of marine environment detection and data collection equipment, directly affects its range and duration.
Xin Tian, Lianhong Zhang, Hongwei Zhang
doaj   +1 more source

Flutter Boundary Prediction of a Two Dimensional Airfoil in Transonic Flight Regime with the Preset Angles of Attack [PDF]

open access: yesXibei Gongye Daxue Xuebao, 2018
Angle of attack has impact on transonic flow filed and aerodynamic force, but most of current researches on flutter use zero angle hypothesis, which has no consideration about angle of attack.

doaj   +1 more source

Research on fixed attack angle attack angle and height flying of hypersonic aircraft [PDF]

open access: yesAdvances in Computer Science Research, 2015
Attack angle is a most important factor that affect the stability of aircraft no matter for supersonic type or hypersonic type aircraft. And height is another factor that will affect the force and moment of the whole dynamic system by change the density of air and finally it will also affect the stability of the whole system. So in this paper a kind of
Junwei Lei, Heng Li, Guangbin Wu
openaire   +1 more source

Thermal Protection Mechanism of a Novel Adjustable Non-Ablative Thermal Protection System for Hypersonic Vehicles

open access: yesAerospace, 2022
In order to improve the thermal protection performance of the active thermal protection system (TPS) based on the spike and jet, an adjustable non-ablative thermal protection system, of which the spike can be rotated in the direction of the free stream ...
Bin Chang, Jie Huang, Wei-Xing Yao
doaj   +1 more source

Analysis of the Magnus Moment Aerodynamic Characteristics of Rotating Missiles at High Altitudes

open access: yesInternational Journal of Aerospace Engineering, 2021
The Magnus moment characteristics of rotating missiles with Mach numbers of 1.3 and 1.5 at different altitudes and angles of attack were numerically simulated based on the transition SST model.
Yihang Xu, Shaosong Chen, Hang Zhou
doaj   +1 more source

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