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Thermal protection and drag reduction with use of spike in hypersonic flow
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What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.1016/0167-6105(82)90011-3openalex-snapshot
von Karman institute for fluid dynamics
inferredcites →https://doi.org/10.1299/jsmefed.2000.35openalex-snapshot
Effect of Spike for Reduction of Hypersonic Aerodynamic Heating
inferredcites →https://doi.org/10.2514/3.30094openalex-snapshot
Effect of a spike on the drag and on the aerodynamic stability of blunt bodies in supersonic flow
inferredcites →https://doi.org/10.2514/8.6977openalex-snapshot
Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight Speeds
What points at this work
Incoming claims: where this work appears in other papers’ reference lists and arguments.
inferred← citeshttps://doi.org/10.1007/978-3-540-85181-3_84openalex-snapshot
Wave drag reduction concept for blunt bodies at high angles of attack
inferred← citeshttps://doi.org/10.1007/978-3-642-25688-2_110openalex-snapshot
Surrogate-Based Multi-objective Aerothermodynamic Design Optimization of Hypersonic Spiked Bodies
inferred← citeshttps://doi.org/10.1007/978-981-13-2490-1_2openalex-snapshot
Numerical Simulation Over Conical Aerospike at Mach 6
inferred← citeshttps://doi.org/10.1007/s00193-018-0868-3openalex-snapshot
On the mechanism of wave drag reduction by concentrated laser energy deposition in supersonic flows over a blunt body
inferred← citeshttps://doi.org/10.1007/s00193-019-00901-7openalex-snapshot
On the location of the laser energy deposition region in wave drag reduction
inferred← citeshttps://doi.org/10.1007/s00231-012-1095-6openalex-snapshot
Numerical heat transfer study around a spiked blunt-nose body at Mach 6
inferred← citeshttps://doi.org/10.1007/s00231-013-1173-4openalex-snapshot
Numerical investigation of drag and heat reduction in hypersonic spiked blunt bodies
inferred← citeshttps://doi.org/10.1007/s42405-025-00953-3openalex-snapshot
Computational Investigation of Aerothermodynamic Characteristics of Spherical and Flat Disc Spiked Blunt Body at Hypersonic Flow
inferred← citeshttps://doi.org/10.1016/b978-0-323-91770-4.00002-1openalex-snapshot
Mechanical techniques (spike)
inferred← citeshttps://doi.org/10.1016/j.actaastro.2013.11.015openalex-snapshot
Aerothermodynamics of generic re-entry vehicle with a series of aerospikes at nose
inferred← citeshttps://doi.org/10.1016/j.actaastro.2016.09.004openalex-snapshot
Experimental investigation on drag and heat flux reduction in supersonic/hypersonic flows: A survey
inferred← citeshttps://doi.org/10.1016/j.actaastro.2020.03.009openalex-snapshot
Hypersonic drag reduction mechanism of a novel combinational spike and multi-opposing jets aerodynamic configuration
inferred← citeshttps://doi.org/10.1016/j.actaastro.2020.03.019openalex-snapshot
Numerical simulation of aerodynamic problems based on adaptive mesh refinement method
inferred← citeshttps://doi.org/10.1016/j.actaastro.2020.08.023openalex-snapshot
Spike root oblique jet effect on drag and heat load reduction performance for hypersonic vehicles
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2014.02.076openalex-snapshot
Investigation of transpiration cooling for sintered metal porous struts in supersonic flow
inferred← citeshttps://doi.org/10.1016/j.ast.2018.01.039openalex-snapshot
Drag reduction investigation for hypersonic lifting-body vehicles with aerospike and long penetration mode counterflowing jet
inferred← citeshttps://doi.org/10.1016/j.ast.2019.01.027openalex-snapshot
Aerodisk effects on drag reduction for hypersonic blunt body with an ellipsoid nose
inferred← citeshttps://doi.org/10.1016/j.ast.2019.04.030openalex-snapshot
Multi-objective design optimization of blunt body with spike and aerodisk in hypersonic flow
inferred← citeshttps://doi.org/10.1016/j.ast.2019.105459openalex-snapshot
Hypersonic flow characteristics and relevant structure thermal response induced by the novel combined spike-aerodome and lateral jet strategy
inferred← citeshttps://doi.org/10.1016/j.ast.2020.105932openalex-snapshot
Assessment on jet direction effect on drag and heat reduction efficiency for hypersonic vehicles
inferred← citeshttps://doi.org/10.1016/j.compfluid.2024.106201openalex-snapshot
Numerical investigation of nonlinear aeroelastic characteristics of a supersonic drag-reduction spike
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2024.108317openalex-snapshot
Active control devices of spiked body for drag and heat flux reduction in supersonic/hypersonic flows: State-of-the-art review
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2025.109109openalex-snapshot
Research on comprehensive parameters of thermal protection and drag reduction devices under hypersonic conditions
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2019.07.035openalex-snapshot
Attached flow formed by opposing jet in hyper/supersonic flow
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2019.119236openalex-snapshot
Parameter study on drag and heat reduction of a novel combinational spiked blunt body and rear opposing jet concept in hypersonic flows
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2022.123592openalex-snapshot
Research on a novel combined shock control mechanism for thermal protection and drag reduction in hypersonic compressible flow field
inferred← citeshttps://doi.org/10.1016/j.ijmecsci.2024.109282openalex-snapshot
Compressible FSI of elastic spikes for drag reduction under hypersonic flow
inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2025.110101openalex-snapshot
Multi-objective design optimization and fluid-thermal coupling analysis on the active flow control induced by a novel aerospike-channel injection concept
inferred← citeshttps://doi.org/10.1016/j.paerosci.2011.06.001openalex-snapshot
Recent advances in the aerothermodynamics of spiked hypersonic vehicles
inferred← citeshttps://doi.org/10.1016/j.paerosci.2016.04.001openalex-snapshot
A review of design issues specific to hypersonic flight vehicles
inferred← citeshttps://doi.org/10.1016/j.paerosci.2018.10.002openalex-snapshot
Research progress on strut-equipped supersonic combustors for scramjet application
inferred← citeshttps://doi.org/10.1016/j.protcy.2016.08.174openalex-snapshot
Computational Study of Hypersonic Flow Past Spiked Blunt Body Using RANS and DSMC Method
inferred← citeshttps://doi.org/10.1017/aer.2017.100openalex-snapshot
Investigation of aerodynamic coefficients at Mach 6 over conical, hemispherical and flat-face spiked body
inferred← citeshttps://doi.org/10.1017/s0001924000002554openalex-snapshot
Experimental investigation on spiked body in hypersonic flow
inferred← citeshttps://doi.org/10.1017/s0001924000003675openalex-snapshot
Numerical simulation of the flow field over conical, disc and flat spiked body at Mach 6
inferred← citeshttps://doi.org/10.1017/s0001924000005893openalex-snapshot
Numerical investigation of aeroheating characteristics of spiked blunt bodies at Mach six flight conditions
inferred← citeshttps://doi.org/10.1017/s0001924000008265openalex-snapshot
Pressure measurements over a hemisphere-cylinder body attached with a forward facing spike
inferred← citeshttps://doi.org/10.1017/s0001924000008587openalex-snapshot
Aerothermodynamics of a hypersonic projectile with a double-disk aerospike
inferred← citeshttps://doi.org/10.1061/(asce)as.1943-5525.0000707openalex-snapshot
Assessment of the Aerodisk Size on Drag Reduction and Thermal Protection of High-Bluntness Vehicles at Hypersonic Speeds
inferred← citeshttps://doi.org/10.1061/(asce)as.1943-5525.0000901openalex-snapshot
Numerical Simulation of Aerodynamic Heating over Solid Blunt Configuration with Porous Spike
inferred← citeshttps://doi.org/10.1061/(asce)as.1943-5525.0001290openalex-snapshot
Nonablative Dual-Jet Strategy for Drag and Heat Reduction of Hypersonic Blunt Vehicles
inferred← citeshttps://doi.org/10.1061/jaeeez.aseng-5809openalex-snapshot
Numerical Study of the Performance of Combined Spike and Transpiration Cooling Concept for Nose Cone under Hypersonic Conditions
inferred← citeshttps://doi.org/10.1063/5.0095284openalex-snapshot
Design and analysis of breathing blunt nose (BBN) with flat-faced aero-disk for drag reduction in supersonic flows
inferred← citeshttps://doi.org/10.1063/5.0177829openalex-snapshot
Flow modification cooling technique to reduce aerodynamic wave drag by mechanical cut shape aero-spike for the blunted body at Mach 8.0
inferred← citeshttps://doi.org/10.1063/5.0182975openalex-snapshot
Numerical investigation of hypersonic flow over 60 degree apex angle blunted cone with flat aerodisk spike: A flow modification technique
inferred← citeshttps://doi.org/10.1063/5.0220407openalex-snapshot
Mechanism of active flow control using a novel spike aerodome-channel concept in the hypersonic flow: A numerical study
inferred← citeshttps://doi.org/10.1063/5.0273538openalex-snapshot
Aerodynamic heat and drag reduction for hypersonic rarefied flow around a bipyramid–type bluff body
inferred← citeshttps://doi.org/10.1080/01457632.2013.837790openalex-snapshot
Numerical Simulation of Transpiration Cooling for Sintered Metal Porous Strut of the Scramjet Combustion Chamber
inferred← citeshttps://doi.org/10.1080/10407782.2024.2302080openalex-snapshot
Heat flux and aerodynamics drag reduction of a hypersonic flow with the different tips of the taper spike design parabolic nose cone
inferred← citeshttps://doi.org/10.1080/10407790.2024.2387266openalex-snapshot
Reducing aerodynamic drag and heat generation in parabolic nose cones using single and double-disc tapered spikes
inferred← citeshttps://doi.org/10.1088/1742-6596/2252/1/012004openalex-snapshot
Research on drag reduction and heat prevention performance of spike with the channel concept for hypersonic blunt body
inferred← citeshttps://doi.org/10.1088/1742-6596/2805/1/012011openalex-snapshot
Numerical investigation on the performance of combinational spike and transpiration cooling concept for nose cone under hypersonic conditions
inferred← citeshttps://doi.org/10.1109/ibcast.2015.7058542openalex-snapshot
Design of spiked hemispherical body in hypersonic flow
inferred← citeshttps://doi.org/10.1109/ibcast59916.2023.10713012openalex-snapshot
Spike-Based Aerodynamic Shape Optimization of Blunt Bodies Using Machine Learning and CFD Techniques
inferred← citeshttps://doi.org/10.1109/icscan.2018.8541144openalex-snapshot
Numerical Simulation Over Flat-Disk Aerospike at Mach 6
inferred← citeshttps://doi.org/10.1109/isscaa.2010.5632258openalex-snapshot
Numerical analysis of thermal protection and drag redunction with use of spike
inferred← citeshttps://doi.org/10.1155/2021/8821721openalex-snapshot
Numerical Simulation of Supersonic Carman Curve Bodies with Aerospike
inferred← citeshttps://doi.org/10.14311/tpfm.2016.012openalex-snapshot
STUDY OF HYPERSONIC FLOW PAST SPIKED BLUNT BODY USING DIRECT SIMULATION MONTE CARLO METHOD
inferred← citeshttps://doi.org/10.21608/asat.2011.23410openalex-snapshot
Aerothermodynamics of Spiked Bodies: Part I
inferred← citeshttps://doi.org/10.21608/asat.2011.23411openalex-snapshot
Aerothermodynamics of Spiked Bodies: Part II
inferred← citeshttps://doi.org/10.2322/jjsass.52.38openalex-snapshot
A Study on Reduction of Aerodynamic Heating by Opposing Jet in Supersonic Flow
inferred← citeshttps://doi.org/10.2322/tastj.10.te_15openalex-snapshot
Hypersonic Flow Investigation of Aerospikes for Delta-type Lifting Body Configurations
inferred← citeshttps://doi.org/10.2322/tastj.14.pe_27openalex-snapshot
Flow Control by Repetitive Discharge for Space Vehicle at High Altitude
inferred← citeshttps://doi.org/10.2514/1.15332openalex-snapshot
Experimental Study on Thermal Protection System by Opposing Jet in Supersonic Flow
inferred← citeshttps://doi.org/10.2514/1.a33370openalex-snapshot
Fluid–Thermal Interaction Investigation of Spiked Blunt Bodies at Hypersonic Flight Condition
inferred← citeshttps://doi.org/10.2514/1.a33414openalex-snapshot
Numerical Analysis of Hypersonic Flow Past Blunt Bodies with Aerospikes
inferred← citeshttps://doi.org/10.2514/1.a33865openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/1.a34459openalex-snapshot
Multi-Objective Design Optimization of Hypersonic Spiked Blunt Body with Opposing Jet
inferred← citeshttps://doi.org/10.2514/1.a35390openalex-snapshot
Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle
inferred← citeshttps://doi.org/10.2514/1.a35757openalex-snapshot
Influence of Nose Cone Fairing and Spike on Supersonic Blunt Body Flows
inferred← citeshttps://doi.org/10.2514/1.a36223openalex-snapshot
Aerodisk Effect on Drag and Heat Reduction of Hypersonic Spiked Blunt Body
inferred← citeshttps://doi.org/10.2514/1.j054757openalex-snapshot
Experimental Investigation on Transpiration Cooling Effectiveness for Spacecraft Entering Martian Atmosphere
inferred← citeshttps://doi.org/10.2514/1.j062826openalex-snapshot
Experimental Investigations on High-Speed Aerodynamic Heating over Inflatable Decelerators
inferred← citeshttps://doi.org/10.2514/6.2003-4041openalex-snapshot
Effect of Pressure Ratio on Aerodynamic Heating Reduction due to Opposing Jet
inferred← citeshttps://doi.org/10.2514/6.2004-2428openalex-snapshot
Some Aerodynamic and Aerothermodynamic Considerations for Reusable Launch Vehicles
inferred← citeshttps://doi.org/10.2514/6.2004-2559openalex-snapshot
Numerical Analyses of Possibility of Flow Control by Energy Deposition
inferred← citeshttps://doi.org/10.2514/6.2005-188openalex-snapshot
Numerical Study of Thermal Protection System by Opposing Jet
inferred← citeshttps://doi.org/10.2514/6.2007-462openalex-snapshot
Application of Pressure-Based Coupled Solver to the Problem of Hypersonic Missiles with Aerospikes
inferred← citeshttps://doi.org/10.2514/6.2008-4000openalex-snapshot
Wave Drag Reduction Approach for Blunt Bodies at High Angles of Attack: Proof-of-Concept Experiments
inferred← citeshttps://doi.org/10.2514/6.2009-325openalex-snapshot
Flow Field Computations Over Conical, Disc and Flat Spiked Body at Mach 6
inferred← citeshttps://doi.org/10.2514/6.2010-991openalex-snapshot
Reducing Aerodynamic Heating by the Opposing Jet in Supersonic and Hypersonic Flows
inferred← citeshttps://doi.org/10.2514/6.2011-2228openalex-snapshot
Heat Transfer Analysis over Disc and Hemispherical Spike Attached to Blunt-Nosed Body at Mach 6
inferred← citeshttps://doi.org/10.2514/6.2013-3114openalex-snapshot
A novel means of dissipation of shock wave induced heat in a high speed flow
inferred← citeshttps://doi.org/10.2514/6.2014-0705openalex-snapshot
Reduction of Aerodynamic Heating with Opposing Jet through Extended Nozzle in High Enthalpy Flow
inferred← citeshttps://doi.org/10.2514/6.iac-05-d2.5.10openalex-snapshot
A New Thermal Protection System by Opposing Jet fo...
inferred← citeshttps://doi.org/10.3390/aerospace13030235openalex-snapshot
Improvement in Efficiency of Blunt Cone Drag and Heat Reduction by Combination of Aerospike and Partition Jets
inferred← citeshttps://doi.org/10.3390/aerospace9120742openalex-snapshot
Aerodisk Effect on Hypersonic Boundary Layer Transition and Heat Transfer of HIFiRE-5 Vehicle
inferred← citeshttps://doi.org/10.3390/e24101325openalex-snapshot
Application of a Gas-Kinetic BGK Scheme in Thermal Protection System Analysis for Hypersonic Vehicles
inferred← citeshttps://doi.org/10.36347/sjet.2024.v12i07.001openalex-snapshot
Numerical Investigations of Flow Field over Conical, Disc and Flat-Face Spiked-Nose Attached to a Hemisphere Body at Mach 6
inferred← citeshttps://doi.org/10.47176/jafm.17.3.2150openalex-snapshot
Evaluation of Various Flow Control Methods in Reducing Drag and Aerodynamic Heating on the Nose of Hypersonic Flying Objects
inferred← citeshttps://doi.org/10.5772/intechopen.74522openalex-snapshot
Heat Transfer Analysis without and with Forward Facing Spike Attached to a Blunt Body at High Speed Flow
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