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                             91 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 A compact normal-mode VHF/UHF dual-band helical antenna for lunar microsatellite Hu, Chaoran

126 C p.
artikel
2 Adaptive NN motion control and predictive coordinate planning for aerial manipulators Cao, Huazi

126 C p.
artikel
3 Aerodynamic shape optimization using a time spectral coupled adjoint for nonlinear aeroelastic problems Prasad, Rachit

126 C p.
artikel
4 A method for the reconstruction of buzz-saw noise source and pressure field in transonic fan with multi-types of blade variations Tang, Xiaolong

126 C p.
artikel
5 Analytical development on impact behaviour of composite sandwich laminates by differentiated loading regimes Chao Correas, A.

126 C p.
artikel
6 An enhanced hybrid deep neural network reduced-order model for transonic buffet flow prediction Liu, Ziyang

126 C p.
artikel
7 A new data assimilation method of recovering turbulent mean flow field at high Reynolds numbers Liu, Yilang

126 C p.
artikel
8 An investigation of hybrid CPU-GPU solvers for supersonic reacting flow simulation with detailed chemical kinetics Rao, Sihang

126 C p.
artikel
9 A novel FEM-FVM coupled method of evaluating the explosion shock wave of a thermobaric bomb on the internal and external flow characteristics of aircraft Mi, Baigang

126 C p.
artikel
10 A novel worm gear actuated repeatable locking/unlocking device for magnetically suspended control moment gyro Ye, Xiangyang

126 C p.
artikel
11 Attitude adaptive control of satellites using double-gimbal magnetically suspended control moment gyros Lungu, Romulus

126 C p.
artikel
12 Buffet boundary prediction using RANS-based criteria and adjoint methods Petrocchi, Andrea

126 C p.
artikel
13 Collision-free formation-containment control for a group of UAVs with unknown disturbances Chen, Lin

126 C p.
artikel
14 Comprehensive performance of multifunctional lightweight composite reinforced with integrated preform for thermal protection system exposed to extreme environment Li, Weijie

126 C p.
artikel
15 Conjugate thermal analysis of X-51A-like aircraft with regenerative cooling channels Han, Dabin

126 C p.
artikel
16 Control of shock-wave/boundary-layer interaction using a backward-facing step Zhai, Jian

126 C p.
artikel
17 Coverage-based cooperative guidance law for intercepting hypersonic vehicles with overload constraint Liu, Shuangxi

126 C p.
artikel
18 Critical endwall blockage attenuation-based automatic optimization of casing treatment design for transonic axial flow compressor Wang, Xuesong

126 C p.
artikel
19 Design and testing of an additively manufactured flameholder for scramjet flows Lieber, Damien A.

126 C p.
artikel
20 Distributed robust adaptive formation control of fixed-wing UAVs with unknown uncertainties and disturbances Zhi, Yongran

126 C p.
artikel
21 Dynamic modeling and robust nonlinear control of a laboratory gas turbine engine Singh, Richa

126 C p.
artikel
22 Dynamic velocity error based trajectory tracking for space robotic manipulator Prakash, Aditya

126 C p.
artikel
23 Editorial Board
126 C p.
artikel
24 Effect of area ratio and heat release method on the Ma∞ = 2-6 operation performance of rocket-based combined cycle engine Yan, De-kun

126 C p.
artikel
25 Effects of a significant boundary layer on the flame acceleration and transition to detonation in millimeter-scale tubes Pan, Zhenhua

126 C p.
artikel
26 Effects of inert dispersed particles on the propagation characteristics of a H2/CO/air detonation wave Zhang, Bo

126 C p.
artikel
27 Effects of jet/flame interaction on deflagration-to-detonation transition by non-reactive gas jet in a methane-oxygen mixture Cheng, Jun

126 C p.
artikel
28 Effects of slat track on the flow and acoustic field of high-lift devices Chen, Guoyong

126 C p.
artikel
29 Ejector mode performance improvement of rocket-based combined cycle engine designed for dual-ramjet mode Yan, De-kun

126 C p.
artikel
30 Electromagnetic field/hypersonic flow field coupled algorithm and its application in the magnetic controlled inlet design Wang, Ding

126 C p.
artikel
31 Energy-based nonlinear adaptive control for collaborative transportation systems Chai, Yi

126 C p.
artikel
32 Enhancing navigation integrity for Urban Air Mobility with redundant inertial sensors Wang, Shizhuang

126 C p.
artikel
33 Evaluation of flamelet/progress variable model for the applications in supersonic combustion using hybrid RANS/LES approach Tang, Tao

126 C p.
artikel
34 Experimental flameholding performance of a scramjet cavity with an inclined front wall Landsberg, Will O.

126 C p.
artikel
35 Experimental investigations of hypersonic inlet unstart/restart process and hysteresis phenomenon caused by angle of attack Xu, Shangcheng

126 C p.
artikel
36 Experimental study of H2/air rotating detonation wave propagation characteristics at low injection pressure Han, Jiaxiang

126 C p.
artikel
37 Experimental study on rocket jet-driven ignition and scramjet combustion in a kerosene-fueled RBCC combustor Shi, Lei

126 C p.
artikel
38 Fast costate estimation for indirect trajectory optimization using Bezier-curve-based shaping approach Huo, Mingying

126 C p.
artikel
39 Film cooling performance on pressure side of turbine blade with different number of hole rows under rotating state Meng, Long

126 C p.
artikel
40 Flight dynamics of aerial vehicle considering time-varying ambient wind Seo, Yongjun

126 C p.
artikel
41 Fluid-structure interaction simulations of the ASPIRE SR01 supersonic parachute flight test Boustani, Jonathan

126 C p.
artikel
42 Fuzzy adaptive sliding mode fault estimation and fixed-time fault-tolerant control for coupled spacecraft based on SE(3) Mei, Yafei

126 C p.
artikel
43 Higher-order hygro-magneto-electro-thermomechanical analysis of FG-GNPs-reinforced composite cylindrical shells embedded in PEM layers Arshid, Ehsan

126 C p.
artikel
44 Higher-order Taylor series expansion for uncertainty quantification with efficient local sensitivity Paudel, Achyut

126 C p.
artikel
45 Hybrid formation control framework for solar-powered quadrotors via adaptive fission pigeon-inspired optimization Yuan, Yang

126 C p.
artikel
46 Ice accretion and aerodynamic effects on a turbofan engine nacelle under takeoff conditions Yang, Qian

126 C p.
artikel
47 Impact localization with a weighted spectral cross correlation method Jiang, Wensong

126 C p.
artikel
48 Impact resistance mechanism of reactive material bumper for spacecraft Whipple shield: Experiments and numerical simulations Ren, Siyuan

126 C p.
artikel
49 Influence of key geometrical features on the non-reacting flow of a Lean Direct Injection (LDI) combustor through Large-Eddy Simulation and a Design of Experiments Carreres, M.

126 C p.
artikel
50 Influence of the rotating direction and speed of controllable speed casing on the flow stability of a transonic compressor rotor under design condition Wu, Wanyang

126 C p.
artikel
51 Investigation of energy accommodation coefficient at gas-solid interface of a hypersonic flying vehicle Han, Quan

126 C p.
artikel
52 Joint routing and charging optimization for eVTOL aircraft recovery Guo, Zhen

126 C p.
artikel
53 Joule heated hot wall models in hypersonic wind tunnel facilities for energy deposition studies Moran, Jeremy H.

126 C p.
artikel
54 Large eddy simulations of unsteady non-reaction flow characteristics using different geometrical combustor models Meng, Nan

126 C p.
artikel
55 Learning-based fixed-wing UAV reactive maneuver control for obstacle avoidance Wu, Jianfa

126 C p.
artikel
56 Mechanical behaviors and fracture mechanisms of CFRP sandwich composite structures with bio-inspired thin-walled corrugated cores Le, Vinh Tung

126 C p.
artikel
57 Mechanism and prediction of flow oscillation based on counter-flow jet for drag reduction in hypersonic flow Kim, Yongchan

126 C p.
artikel
58 Missile aerodynamic shape optimization design using deep neural networks Wu, Pin

126 C p.
artikel
59 Modeling liquid rocket engine coolant flow and heat transfer in high roughness channels Latini, Beatrice

126 C p.
artikel
60 Multi-channel gliding arc plasma-assisted ignition in a kerosene-fueled model scramjet engine Feng, Rong

126 C p.
artikel
61 Neural network disturbance observer with extended weight matrix for spacecraft disturbance attenuation He, Tongfu

126 C p.
artikel
62 Nonlinear damping model for supersonic air-intake buzz Suryanarayana, G.K.

126 C p.
artikel
63 Nonlinear homogeneous sliding mode approach for fixed-time robust formation tracking control of networked quadrotors Mechali, Omar

126 C p.
artikel
64 Numerical and experimental investigation of a radially reduced diffuser design concept for a centrifugal compressor performance at design point McLaughlin, Laura

126 C p.
artikel
65 Numerical-experimental evaluation and modelling of aerodynamic ground effect for small-scale tilted propellers at low Reynolds numbers Garofano-Soldado, Ambar

126 C p.
artikel
66 Numerical investigations on the beating behavior of self-excited combustion instability in a hydrogen-fueled Rijke type combustor Song, Xiuyang

126 C p.
artikel
67 Numerical simulations of a rotor in confined areas including the presence of wind Merabet, Reda

126 C p.
artikel
68 Numerical study of back-propagation suppression and intake loss in an air-breathing pulse detonation engine Wang, Zhiwu

126 C p.
artikel
69 Numerical study of the hysteresis effect on the supercritical airfoil for the transonic circulation control Wang, Qing

126 C p.
artikel
70 Numerical study of unsteady flow and cooling characteristics of turbine blade cutback trailing edges integrated with pin fins and film holes Li, Yuefeng

126 C p.
artikel
71 Optimal V ∞ leveraging maneuvers using gray solar sail Quarta, Alessandro A.

126 C p.
artikel
72 Output- and state-dependent Riccati equation: An output feedback controller design Nekoo, Saeed Rafee

126 C p.
artikel
73 Pressure-sensitive paint integrated with digital image correlation for instantaneous measurement on rotating blades Dong, Zhe

126 C p.
artikel
74 Quasi-wall-resolved large eddy simulation of transitional flow in a transonic compressor rotor Li, Zhen

126 C p.
artikel
75 Reduction of feedback pressure perturbation for rotating detonation combustors Ji, Zifei

126 C p.
artikel
76 Revised semi-empirical aerodynamic estimation for modelling flight dynamics of an airship Suvarna, Sohan

126 C p.
artikel
77 Rigid-flexible coupling dynamic modeling and analysis of dumbbell-shaped spacecraft Wang, Boyang

126 C p.
artikel
78 Robust backstepping sliding mode aircraft attitude and altitude control based on adaptive neural network using symmetric BLF Singh, Prabhjeet

126 C p.
artikel
79 Simultaneous aircraft sizing and multi-objective optimization considering off-design mission performance during early design Cai, Yu

126 C p.
artikel
80 Spinning pulsed detonation in rotating detonation engine Shen, Dawen

126 C p.
artikel
81 Studies on a swirling heptane spray flame by large-eddy simulation Zhou, Lixing

126 C p.
artikel
82 Study on propagation mechanisms of the actuations generated by plasma synthetic jet actuator in a supersonic flow Zhang, Weilin

126 C p.
artikel
83 Surrogate modelling for an aircraft dynamic landing loads simulation using an LSTM AutoEncoder-based dimensionality reduction approach Lazzara, Michele

126 C p.
artikel
84 System identification method based on interpretable machine learning for unknown aircraft dynamics Cao, Rui

126 C p.
artikel
85 Theoretical and numerical analysis of effects of sudden expansion and contraction on compressible flow phenomena in Hyperloop system Kim, Jihoon

126 C p.
artikel
86 Thermal performance in latticework ducts with various endwall shapes for aero-craft turbine cooling Luo, Lei

126 C p.
artikel
87 Three-dimensional field of view and impact angle constrained guidance with terminal speed maximization Duvvuru, Ramesh

126 C p.
artikel
88 Unknown input observer-based appointed-time funnel control for quadrotors Zhang, Wenhao

126 C p.
artikel
89 Unsteady response of performance for centrifugal compressor under pulsating backpressure condition Yang, Mingyang

126 C p.
artikel
90 Updated conceptual design of hydrogen/ethylene fueled detonation ramjet: Test fires at Mach 1.5, 2.0, and 2.5 Ivanov, V.S.

126 C p.
artikel
91 Wing-in-ground craft longitudinal modeling and simulation based on a moving wavy ground test Wang, Lixin

126 C p.
artikel
                             91 gevonden resultaten
 
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