Proceedings of the Institution of Mechanical Engineers Part G-Journal

Papers
(The TQCC of Proceedings of the Institution of Mechanical Engineers Part G-Journal is 3. The table below lists those papers that are above that threshold based on CrossRef citation counts [max. 250 papers]. The publications cover those that have been published in the past four years, i.e., from 2021-05-01 to 2025-05-01.)
ArticleCitations
New approach of inverse design of transonic compressor rotor blade via prescribed isentropic Mach distributions without modification of governing equations22
Effects of Coanda jet direction on the aerodynamics and flow physics of the swept circulation control wing15
Investigation of variable geometry orifice design for improving centrifugal compressor low-end performance and stable operating range15
Effect of pre-swirl nozzle closure modes on unsteady flow and heat transfer characteristics in a pre-swirl system of aero-engine15
Effects of fusion height of tip winglet on the clearance flow in a compressor cascade14
Design and performance evaluation of a novel H2/O2 electro-chemical hybrid thruster13
Real-time prediction for the surge of turboshaft engine using multi-branch feature fusion neural network13
Soft one-class extreme learning machine for turboshaft engine fault detection11
Pipeline fault simulation and control of a liquid rocket engine10
Analytical trajectory prediction for skip re-entry of lifting vehicle10
Adaptive interacting multiple model particle filter based on a dual-pattern bat algorithm for maneuvering target tracking10
Optimal flight trajectory synthesis for an anti-collision maneouvre performed within environment of moving obstacles10
Nonlinear combustion instability analysis of a bluff body burner based on the flame describing function10
Adaptive fault-tolerant flutter control considering related failure10
Model predictive control–based compound control strategy for ducted rockets gas flow with anti-regulation suppression10
A method for fault diagnosis of power system of carrier rocket engine based on linear-quadratic receding time-domain algorithm9
Propulsive and combustion behavior of hydrocarbon fuels containing boron nanoparticles in a liquid rocket combustor9
Optimization of kinematic parameters of dragonfly wing section in forward flapping flight9
Steam turbine high-pressure reaction stages; new 3D vortices breakdown and airfoil optimization method9
Multi-objective nozzle design optimization for maximum thrust vectoring performance9
Model-based adaptive synergetic control of a UAV manipulator9
Effect of flash boiling on the spray characteristics of pressure swirl spray nozzles using liquid nitrogen9
Adaptive super-twisting control for deployment of space-tethered system with unknown boundary disturbances9
Integrated control scheme for a large membrane diffractive space telescope9
Robust sliding mode augmenting integral backstepping for lateral-directional control of a highly maneuverable aircraft9
Effects of canard oscillations on the unsteady flowfield over the wing in supersonic flow9
Variable-horizon predictive tracking control for air-breathing hypersonic vehicle based on composite disturbance observer9
Robust adaptive quadrotor position tracking control for uncertain and fault conditions8
Flight dynamics analysis of a small tandem helicopter considering aerodynamic interference8
Study on the test load for the structural test of the flight-load condition of the external fuel tank for fixed-wing aircraft8
High-altitude airship variable-pitch propeller performance analysis at multiple altitudes8
Effect of load distribution of the front and rear blades on the flow characteristics of highly loaded subsonic compressor tandem cascades8
A novel interactive robust filter algorithm for GNSS/SINS integrated navigation8
A flexible method for geometric design of axial compressor blades8
Effect of circumferential non-uniform tip clearance on the dynamic stall process of a single-stage axial compressor with total pressure distortion8
Optimization of transonic low-Reynolds number airfoil based on genetic algorithm7
Experimental investigation on the ignition limits of a kerosene-fueled cavity in model scramjet combustor7
Optimization of low-thrust multi-debris removal mission via an efficient approximation model of orbit rendezvous7
Straight-line path-following control for roll-out phase of the equipped-skid aircraft7
Development of a novel autonomous space debris collision avoidance system for uncrewed spacecraft7
Novel model reference adaptive control with application to wing rock example7
Air curtain as a SARS-CoV-2 spreading mitigation method in a small aircraft cabin7
Conceptual aero-structural design of a fan stage under distorted flow6
A novel hybrid aircraft propulsion based on the DEA compressor—part B: Performance6
Integrated entry guidance with no-fly zone constraint using reinforcement learning and predictor-corrector technique6
Modified circular curve-based impact angle control guidance6
Nonlinear model predictive control for aircraft flat-spin recovery6
Coordinated control of free-floating dual-arm space robots based on hybrid task-priority approach6
Proof of concept study on a self-driven pulsed jet on a compressor stator blade by numerical simulation6
Intake grille design for an embedded ventilation-and-cooling system in an aircraft6
Influence of bioinspired morphing on the flow field characteristics of UAV wings at low Reynolds number6
Effect of the trailing-edge flap on tones due to self-excited oscillation within the leading-edge slat cove6
The response of the solid fuel ramjet combustor to the inflow excitations6
Fixed-time cooperative guidance for multiple missiles with impact angle constraint6
Finite-time convergent control for spacecraft attitude stabilization based on the adding power integrator technique6
Sensor fault-tolerant attitude determination system based on the nonlinear interacting-multiple-model approach6
Adaptive second order sliding mode guidance law for missile-target interception with fuzzy logic system6
Structural dynamic response analysis due to the slit flow between the tailplane and the elevator6
Comparison between two computational fluid dynamics methods for gust response predictions5
Effect of upper surface shape on waverider performances5
Design optimization of a morphing winglet for all flight missions of a civil aircraft5
Practical actuator fault detection, identification, and accommodation for a quadrotor with arbitrary faults through direct computation of thrusts5
Mechanism of characteristic change of panel flutter caused by oblique shock impingement5
Path-following control of an underactuated stratospheric airship with unknown dynamics and external disturbances using time-delay control5
Experimental method for the planar landing of a three-legged asteroid probe: The effects of asymmetric configuration and element forces5
A model-based design methodology for flight control systems: Global 7500 pitch control case study5
An unsteady two-dimensional vortex method for the flow separation over a flapping wing5
Early warning and thickness measurement of aircraft icing using ultrasonic pulse echoes5
Mathematical modeling of an articulated flying vehicle for precise control analysis in grasping highly oscillatory objects5
Bounded distance control for Multi-UAV formation safety and preservation in target-tracking applications5
Numerical investigation of the effect of triangular cavity on the unsteady aerodynamics of NACA 0012 at a low Reynolds number5
Numerical solution of spacecraft pursuit-Evasion-Capture game based on progressive shooting method5
Multi-objective aerodynamic optimization using active multi-output Gaussian process and mesh deformation method5
Research on the roll control of the flapless aircraft with circulation control5
Investigation of the effects of flame surface development on the ignition mechanism of aero-engine combustors5
Research on the flow field and film cooling effectiveness of the endwall with swirling film cooling5
Effects of spin rate on the surface pressure distribution of a rotating model5
Nonlinear vibrations analysis of two-directional functionally graded porous cylindrical shells resting on elastic substrates in a thermal environment based on Donnell nonlinear shell theory4
Design of sliding mode flight control system for a flexible aircraft4
Maneuvering penetration strategies of ballistic missiles based on deep reinforcement learning4
Velocity-free fixed-time attitude tracking fault-tolerant control for rigid spacecraft based on the homogeneity method4
A multi-parameter stable-distribution-based protection levels calculation method for ground-based augmentation systems integrity assessment4
Design studies for a light aircraft wing with highly integrated load-bearing hydrogen tanks using multi-objective optimization methods4
Synchronous flying-around control for uncontrolled tumbling spacecraft4
An innovative integrated path planning and trajectory tracking framework for a quadrotor slung load system in an urban environment4
Cascade-modified uncertainty and disturbance estimator–based control of quadrotors for accurate attitude tracking under exogenous disturbance4
Feasibility study of carbon-fiber reinforced polymer linerless pressure vessel tank4
A modified unsteady-nonlinear aeroelastic model for flapping wings4
The effects of spacing to diameter ratio on mixing characteristics of circular and elliptical twin jets4
A review of aircraft environmental control system simulation and diagnostics4
Re-understanding and improvement of the pseudo-spectral method for rapid footprint generation4
Nonlinear performance of aerospace face gear-planetary gear transmission system under multi-factors including the effect of temperature4
Numerical investigation of the influence of aerothermoelastic dynamic response on the performance of the three-dimensional hypersonic inlet4
Design optimization and power management of a fuel cell-battery fixed-wing electric UAV4
Formation generation and visual simulation verification for quadrotors based on time-segmented trajectory planning4
Acoustic velocity analogy formulation for sources in quiescent medium4
Sliding mode controller based aircraft automatic landing for alternate profiles4
Effect of three non-axisymmetric stator schemes on compressor performance with distorted inlet4
Numerical analysis on the conceptual design of an air-breathing engine inlet working in mach number 3∼5.54
A hybrid methodology for knowledge organization and application of Chinese civil aviation regulations from mission safety support perspective4
Fault-tolerant consensus of nonlinear agents considering switching topology in the presence of communication noise4
Feedback linearization-based model reference adaptive control for multirotor UAVs under uncertainties from fuel and payload4
Numerical analysis of aerodynamic characteristics of multi-pod hyperloop system4
Investigation on a new type of latching mechanism on the satellite-rocket docking system and locking dynamic analysis4
Civil aircraft structural maintenance decision using case-based reasoning and LSI4
Dynamic quantitative measurement of ice density by ultrasonic pulse echo4
An approach of Proper Orthogonal Decomposition-aided Free-form Deformation with application in compressor blade design4
Numerical investigation of the effects of turbulence intensity and turbulence length scale on the flow field of high-pressure turbine blade cascades3
Experimental investigation on the performance degradation of helicopter rotor due to ice accretion3
Flight parameter prediction for high-dynamic Hypersonic vehicle system based on pre-training machine learning model3
Turbine inlet temperature effects on the start process of an expansion cycle liquid propellant rocket engine3
Innovative design of modular pantograph tensegrity deployable cylindrical reflectors3
Evaluating one engine inoperative conditions in subscale electric vertical take-off and landing aircraft: An in-depth tethered hover test analysis3
Experimental and numerical research on flow characteristics of inlet particle separator for aero-engine under the influence of water film3
A novel hybrid aircraft propulsion based on the DEA compressor—Part A: Design3
Iterative learning NARMA-L2 control for turbofan engine with dynamic uncertainty in flight envelope3
Investigations on electromagnetic scattering characteristics of aircraft rudder considering electromagnetic discontinuities3
A novel solution methodology for longitudinal flight characterization of a Flying-Wing Micro Aerial Vehicle3
Zero-sum differential game guidance law for missile interception engagement via neuro-dynamic programming3
A response surface equation for the drag polar for an airplane flying in the vicinity of wavy sea surface3
Characterization modeling of wake vortex circulation decay under reasonable worst case conditions with cuckoo search algorithm3
An investigation on LQR based optimal terminal states control for exo-atmospheric flight of super heavy hypersonic intercontinental ballistic missiles using Gauss pseudospectral method3
An optimization method of electrostatic sensor array based on Kriging surrogate model and improved non-dominated sorting genetic algorithm with elite strategy algorithm3
A novel full-electric aircraft propulsion based on the DEA compressor3
A hybrid trim strategy for coaxial compound helicopter3
Impact of internal lattice structures on the weight and natural frequencies of a low pressure turbine blade3
Development and flight test of a manned electric propulsion lightweight airplane3
Experimental research on operation performance and acoustic behavior of two-phase dual-tube pulse detonation engine3
Loss evaluation and aerodynamics investigation of an aggressive intermediate turbine duct under off-design conditions3
Base drag estimation in suddenly expanded supersonic flows using backpropagation genetic and recurrent neural networks3
The cubic pitching moment coefficient of spin-stabilized projectiles3
Robust nonlinear guidance strategies for survival of cooperating unmanned aerial vehicles against pursuing attackers3
Clocking effects on aerodynamics of a gas turbine low pressure axial turbine, part 2: Unsteady simulation3
Aerodynamic performance characterization of bio-inspired wings with leading edge tubercles at low Reynolds number3
Modular reconfigurable rotorcraft for autonomous cargo delivery3
Integral-based robust LPV control of nonlinear flight systems3
Mathematical modeling and experimental investigation of pressure characteristics inside the pilot stage of the deflector jet servo valve considering secondary jet velocity distribution3
Extended aeroacoustic spanwise correction method for the aerodynamic noise prediction of large-span objects3
Cooperative target estimation of strap-down missiles considering random measurement delay3
Comparison of the Newton–Raphson Method and genetic algorithm solutions for nonlinear aircraft trim analysis3
Integrated design of adaptive fault-tolerant control for non-minimum phase hypersonic flight vehicle system with input saturation and state constraints3
Adaptive control of hypersonic vehicles using intelligent allocation3
Robust trajectory tracking of an uncertain quadrotor with almost global finite-time convergence3
Tracking and vibration control of a free-floating space manipulator system with flexible links and joints3
High-efficiency hybrid trim method for CFD simulation of rigid coaxial rotor3
Controlling sonic rectangular jet with nozzle trailing edge modification3
Effects of crosswinds and tip configurations on the initial phase of wingtip vortex evolution3
Variations of supersonic combustion modes induced by different wall temperatures in axisymmetric scramjet3
Design of contingency point return trajectory in the lunar orbit insertion phase for crewed lunar exploration missions3
Blunt hub affecting the radar cross section of rotor based on dynamic scattering method3
Insight into the significance of relative humidity on Nusselt number of crossflow heat exchangers with staggered elliptic tubes3
Stagnation heat flux estimation in spherically blunt axisymmetric hypersonic models3
Optimal prescribed-time attitude tracking for multiple spacecraft systems based on adaptive critic algorithm3
Attitude path design and adaptive robust tracking control of a remote sensing satellite in various imaging modes3
Research on a backstepping flight control method improved by STFT in atmospheric disturbance applications3
Static roughness element effects on protuberance full-span wing at micro aerial vehicle application3
A novel deep-learning-based pressure distribution prediction approach of airfoils3
Predefined-time attitude takeover control of spacecraft with quantized states3
Study on the total pressure and total temperature distortion of axial flow compressor based on different rain ingestion forms3
Aerothermodynamic analysis and rear wake assessment of shock wave interference over blunt leading edge at Mach 6.53
Robust adaptive sliding mode control strategy of uncertain nonlinear systems3
A general real-time optimization framework for polynomial-based trajectory planning of autonomous flying robots3
Inverse dynamics based aerodynamic, gyroscopic, and rotor effects’ compensation in constrained trajectory synthesis for multi-copters3
Co-design of active vibration control and optimal sensor and actuator placement for a flexible wing using reinforcement learning3
Suppression of ground resonance in rotorcraft using active landing gear3
Study of the influence of multiple factors on the boundary layer of a high-lift LPT with the RBF-GA method3
Design and dynamics of a 2PSS+PSR+SP+RUPUR-type parallel rotor of helicopter3
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