Aeronautical Journal

Papers
(The TQCC of Aeronautical Journal is 2. 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 2021-04-01 to 2025-04-01.)
ArticleCitations
Potential of surrogate modelling in compressor casing design focussing on rapid tip clearance assessments87
A spacetime formulation for unsteady aerodynamics with geometry and topology changes26
On the conditions for absolute minimum fuel burn for turbofan powered, civil transport aircraft and a simple model for wave drag22
Investigating the crumpling effect in honeycomb sandwich panels under bending loads using FEA technique20
On the performance of highly aggressive inter compressor ducts20
Key deviation source diagnosis of complex thin-walled structures based on complex networks and weighted transfer entropy20
Assessing evidence-based training in a collaborative virtual reality flight simulator19
Towards intermediate complexity modelling of contrail formation: the new dynamical framework RadMod19
Priority-based intelligent resolution method of multi-aircraft flight conflicts18
The oscillating vortex generator: a boundary layer propulsion and flow control device18
Bespoke stability analysis tool in next-generation computational fluid dynamics solver18
Three-dimensional finite-time guidance law based on sliding mode adaptive RBF neural network against a highly manoeuvering target16
Transit passenger-oriented optimisation of arrival aircraft sequencing15
Computational validation and system identification modeling for stability and control predictions13
Adaptive backstepping fault-tolerant control for hypersonic aircraft with unknown control direction under actuator and sensor faults12
Quantitative flow diagnostics of shock trains by rainbow schlieren deflectometry12
Signal corrector and decoupling estimations for UAV control12
AER volume 125 issue 1289 Cover and Front matter10
Damper model identification using mixed physical and machine-learning-based approach9
Flow Simulation of the Flight Manoeuvres of a Large Transport Aircraft with Load Alleviation – ERRATUM9
Improving pilots’ tactical decisions in air combat training using the critical decision method8
Enhancing the take-off performance of hypersonic vehicles using the improved chimp optimisation algorithm8
Verification framework for control theory of aircraft8
Compliant mechanism design of combined aircraft wing for stable separation8
Numerical investigation of the dynamic stall reduction on the UAS-S45 aerofoil using the optimised aerofoil method8
Disturbance observer-based fixed-time control for hypersonic morphing vehicles with uncertainties8
Effects of blowing upon dynamic stability of blunt nosed re entry vehicles pitching in hypersonic flow8
A numerical approach to evaluate temperature-dependent peridynamics damage model for destructive atmospheric entry of spacecraft7
AER volume 125 issue 1293 Cover and Front matter7
Analysis and modelling of airport resilience, robustness, and vulnerability: impact of COVID-19 pandemic disease7
Wind tunnel test of full-scale wing-propeller system of a eVTOL aircraft7
Influence of clearance and structural coupling parameters on shimmy stability of landing gear7
Aeroengine transient performance simulation integrated with generic heat soakage and tip clearance model7
Enhanced backstepping control for an unconventional quadrotor under external disturbances6
The flight efficiency analysis on the Multi-Arrival Route Point Merge System6
Experimental analysis of noise disturbances generated by reaction wheel6
Certification considerations for the configuration of a hydrogen-fuelled aeroplane6
Adaptive sliding mode attitude control of quaternion model for aircraft based on neural network minimum parameter learning method6
Accuracy of high-order, discrete approximations to the lifting-line equation6
Design and performance of directional rectification control system in an aircraft with a novel type of wheel-ski landing gear6
Shock train response to pulse backpressure forcing6
Actuator fault modeling and fault-tolerant tracking control of multi-vectored propeller aerostat6
Embedded magnetorquer for the more demanding multi-cube small satellites6
Dual-solver hybrid computational approaches for design and analysis of vertical lift vehicles6
Multi-objective reward shaping for global and local trajectory planning of wing-in-ground crafts based on deep reinforcement learning6
The aerodynamic force estimation of a swept-wing UAV using ANFIS based on metaheuristic algorithms6
Unsteady numerical investigation on gas ingestion into the rotor-stator disk cavities of a 1.5-stage turbine5
Eye-tracking analysis to assess the mental load of unmanned aerial system operators: systematic review and future directions5
Non-overshooting sliding mode for UAV control5
Single channel digital controller design for a high spinning rate rolling airframe missile5
An estimation method for the fuel burn and other performance characteristics of civil transport aircraft; part 3 full flight profile when the trajectory is specified5
Performance analysis of power conditioning and distribution module for microsatellite applications5
Distributed planning method for detection array of UAV formation with bearing-only sensor network5
Vision geometry-based UAV flocking5
Combustion characteristics of sustainable aviation fuels in a scaled-down afterburner test rig5
Aircraft takeoff speed prediction with machine learning: parameter analysis and model development5
Quality inspection and error correction of fork-ear type wing-fuselage docking assembly based on multi-camera stereo vision5
Reinforcement learning-adaptive fault-tolerant IGC method for a class of aircraft with non-affine characteristics and multiple uncertainties – CORRIGENDUM5
Distributed digital twins for health monitoring: resource constrained aero-engine fleet management5
A hybrid optimisation method for intercepting satellite trajectory based on differential game4
Attitude maneuver planning and robust tracking control for flexible satellite4
Reinforcement learning-adaptive fault-tolerant IGC method for a class of aircraft with non-affine characteristics and multiple uncertainties4
Cooperative trajectory shaping guidance law for multiple anti-ship missiles4
An extended invariant approach to laminate failure of fibre-reinforced polymer structures4
Spacecraft attitude control based on generalised dynamic inversion with adaptive neural network4
Stability criteria of Samara-like decelerator in unsteady transitions4
A novel approach to runway overrun risk assessment using FRAM and flight data monitoring4
Safety-II: Building safety capacity and aeronautical decision-making skills to commit better mistakes4
Simulation framework and development of the Future Systems Simulator4
Improving real-time drone detection for counter-drone systems4
Neural network-based velocity-controllable UAV flocking4
Research on improvement and optimisation of modelling method of China’s civil aircraft market demand forecast model4
Three-dimensional robust nonlinear cooperative guidance law for spatiotemporal coordination under stringent input constraint4
Multidisciplinary design optimisation of a fully electric regional aircraft wing with active flow control technology4
Propulsion system integration for a first-generation hydrogen civil airliner?4
Propeller control for takeoff of a heavily loaded coaxial compound helicopter4
Historical development of the coaxial contra-rotating propeller4
In-orbit results from the attitude determination and control system of ALSAT-2B3
Verification & validation of lifting line - and -formulations for 3-D planforms under viscous flows3
A stochastic programming model for the aircraft sequencing and scheduling problem considering flight duration uncertainties3
Relative rotor phasing for multicopter vibratory load minimisation3
Transonic small disturbance unsteady potential flow over very high aspect ratio wings3
A methodology to determine the precision uncertainty in gas turbine engine cycle models3
Effect of process parameters on the corrosion characteristics of friction stir welded aluminum alloy AA2014-T63
Frederick W. Lanchester and Aerodynamics: why an automotive engineer wrote a book for aerodynamic education3
Numerical investigations on the effect of blade tip winglet on leakage flow loss reduction for a zero inlet swirl turbine rotor3
Distributed cooperative guidance law without numerical singularity with field-of-view angle constraint3
On the effect of inter compressor duct length on compressor performance3
AER volume 125 issue 1287 Cover and Back matter3
Effect of laser drilling process on combustor liner effusion hole quality3
Aerodynamic characteristics of different configurations of mechanically deployable aerodynamic decelerator in subsonic region3
AER volume 125 issue 1291 Cover and Front matter3
Simulation of the orbital decay of a spacecraft in low Earth orbit due to aerodynamic drag3
A folding wing system for guided ammunitions: mechanism design, manufacturing and real-time results with LQR, LQI, SMC and SOSMC3
Plasma preheating technology for replicating planetary re-entry surface temperatures3
Study on electric towing tractor quantity based on cellular automata3
An unsteady aerodynamic model for three-dimensional wing based on augmented lifting-line method3
GNSS interference detection: Methodology utilising ADS-B NACp indicator and GPS almanac data3
Experimental investigation on droplet evaporation characteristics during combustion of future and current aviation fuels with range of properties3
AER volume 125 issue 1291 Cover and Back matter3
The Australian International Aerospace Congress AIAC 19/203
Ground collision avoidance system with multi-trajectory risk assessment and decision function3
Development of a theoretical model of pilot decision making with conflicting information3
Analysis of modern fan manufacturing variations and their links to Jet-engine performance3
Multiple unmanned aerial systems collision impacts on wing leading edge3
Model compensation control of composite vertical take-off and landing UAV3
Foreword: John Stollery CBE HonFRAeS3
Runway assignment optimisation model for Istanbul Airport considering multiple parallel runway operations3
An alternative approach to evaluate fuel/air mixing quality3
Adaptive reinforcement learning control for a class of missiles with aerodynamic uncertainties and unmodeled dynamics2
Improving the management of air traffic congestion during the approach phase2
Integration of CFO-based three-dimensional target manoeuver compensation guidance rate and transition region optimisation algorithm2
Infrared radiation characteristics of an aero-engine binary plug nozzle with various slot cooling configurations2
Capacity assessment of vertiports with a scheduling algorithm considering quality of service2
Aircraft resilience to GNSS jamming and impact on ADS-B quality indicators2
Analysis of the vortex-dominated flow field over a delta wing at transonic speed2
A fuzzy model to predict the mechanical characteristics of friction stir welded joints of aluminum alloy AA2014-T62
Output constrained neural adaptive control for a class of KKVs with non-affine inputs and unmodeled dynamics2
Fixed-time control for free-floating space manipulators with prescribed constraints and input saturation2
Artificial neural network for preliminary design and optimisation of civil aero-engine nacelles2
A non-linear unsteady vortex-lattice method for rotorcraft applications2
Effect on damage of aircraft windshield impacted by light UAV with different postures2
Numerical simulation of the pressure characteristics of the pulsed jet actuator2
Effect of fuels, aromatics and preparation methods on seal swell2
Numerical investigation of thermochemical non-equilibrium effects in Mach 10 scramjet nozzle2
Multiple model fault diagnosis and fault tolerant control for the launch vehicle’s attitude control system2
Battery consumption estimation methodology for electric unmanned aerial systems2
Impact of actuation and sensor measurement delays on stability of real-time hybrid aeroelastic simulation system2
Numerical analysis of the impact of release timing on trajectory in internal store separation2
Modeling sector route segment capacity under convective weather based on machine learning – CORRIGENDUM2
Application of wavy leading edge to enhance winglet aerodynamic performance2
Numerical investigation of the breakup mode and trajectory of liquid jet in a gaseous crossflow at elevated conditions2
Post Nubes Lux2
Fundamental considerations in the design and performance assessment of propulsive fuselage aircraft concepts2
Investigation on frequency influence on the transverse pulsed jet in a supersonic crossflow2
A framework for optimising flight efficiency of a crossing waypoint by balancing flight conflict frequency and flight-level usage benefits2
Methodology for shape prediction and conversion of a conventional aerofoil to an inflatable baffled aerofoil2
Fixed-time anti-saturation control with concise system structure for the 6-DOF motion of spacecraft2
Base heating and stage separation of launch vehicles2
Static and dynamic characteristics of supersonic cruise missile with damaged wing2
The RAeS 2023 written paper prizes2
Effects of backpressure on unstart and restart characteristics of a supersonic inlet2
On the multi-fidelity approach in surrogate-based multidisciplinary design optimisation of high-aspect-ratio wing aircraft2
A super-convergent thin-walled 3D beam element for analysis of laminated composite structures with arbitrary cross-section2
Historical Development of the Coaxial Contra-Rotating Propeller – CORRIGENDUM2
Elaboration and outlook for metal hydride applications in future hydrogen-powered aviation2
Parametric cost estimation models of civil aircraft for the preliminary aircraft design phase2
Aerothermal and aerodynamic characteristics of reusable hypersonic vehicles with heat transfer minimised sweepback2
Experimental studies on the Hartmann tube2
A dimensionality reduction approach in helicopter level flight performance testing2
Thermal management system design for a series hybrid-electric propulsion architecture2
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