On the public citation graph
Drag reduction of supersonic blunt bodies using opposing jet and nozzle geometric variations
0 signed · 100 inferred · view as graph
Inferred edges come from two machine sources: sweeps of open repository metadata (mostly SSRN and Zenodo), and a bulk OpenAlex citation snapshot. Every row below is labelled with the one it came from. Neither is a complete citation index — absence here is not evidence of absence.
Is this your work? Sign in with ORCID and put your name on the
claims that are yours.
Reference health. See whether every reference in this work resolves to a
known work and none has been retracted — and get a dated CiteStamped
badge you can embed.
What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.1016/j.ast.2015.01.029openalex-snapshot
Drag and heat reduction mechanism in the combinational opposing jet and acoustic cavity concept for hypersonic vehicles
inferredcites →https://doi.org/10.1016/j.cja.2013.02.005openalex-snapshot
Investigation of thermal protection system by forward-facing cavity and opposing jet combinatorial configuration
inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2009.02.035openalex-snapshot
Film cooling at hypersonic Mach numbers using forward facing array of micro-jets
inferredcites →https://doi.org/10.1017/s0022112060000694openalex-snapshot
An experimental investigation of the effect of ejecting a coolant gas at the nose of a bluff body
inferredcites →https://doi.org/10.1017/s0022112066001277openalex-snapshot
The flow of a jet from a body opposing a supersonic free stream
inferredcites →https://doi.org/10.1080/19942060.2010.11015306openalex-snapshot
Computational Study of Drag Reduction at Various Freestream Flows Using a Counterflow Jet from a Hemispherical Cylinder
inferredcites →https://doi.org/10.2514/1.15332openalex-snapshot
Experimental Study on Thermal Protection System by Opposing Jet in Supersonic Flow
inferredcites →https://doi.org/10.2514/1.30084openalex-snapshot
Dynamics of Shock Dispersion and Interactions in Supersonic Freestreams with Counterflowing Jets
inferredcites →https://doi.org/10.2514/2.2819openalex-snapshot
Hypersonic Drag and Heat-Transfer Reduction Using a Forward-Facing Jet
inferredcites →https://doi.org/10.2514/3.28277openalex-snapshot
An experimental investigation of stagnation- point injection
inferredcites →https://doi.org/10.2514/6.1970-219openalex-snapshot
The effects of retrorockets on the aerodynamic characteristics of conical aeroshell planetary entry vehicles
inferredcites →https://doi.org/10.2514/6.2003-4041openalex-snapshot
Effect of Pressure Ratio on Aerodynamic Heating Reduction due to Opposing Jet
inferredcites →https://doi.org/10.2514/6.2005-188openalex-snapshot
Numerical Study of Thermal Protection System by Opposing Jet
inferredcites →https://doi.org/10.2514/6.2010-5048openalex-snapshot
Comparison of Inviscid and Viscous Aerodynamic Predictions of Supersonic Retropropulsion Flowfields
inferredcites →https://doi.org/10.2514/6.2010-991openalex-snapshot
Reducing Aerodynamic Heating by the Opposing Jet in Supersonic and Hypersonic Flows
inferredcites →https://doi.org/10.2514/6.2013-3114openalex-snapshot
A novel means of dissipation of shock wave induced heat in a high speed flow
inferredcites →https://doi.org/10.2514/6.2014-0705openalex-snapshot
Reduction of Aerodynamic Heating with Opposing Jet through Extended Nozzle in High Enthalpy Flow
inferredcites →https://doi.org/10.36884/jafm.3.01.11875openalex-snapshot
Numerical Simulation of Interaction of Sonic Jet with High Speed Flow over a Blunt Body using Solution Mapped Higher Order Accurate AUSM+-UP Based Flow Solver
What points at this work
Incoming claims: where this work appears in other papers’ reference lists and arguments.
inferred← citeshttps://doi.org/10.1007/s12206-022-0524-9openalex-snapshot
Effect of opposing jet on aerodynamic and flight stability characteristics of a generic supersonic slender forebody
inferred← citeshttps://doi.org/10.1007/s12650-021-00773-zopenalex-snapshot
Observation of unsteady motion induced by counterflow jet on blunt body in hypersonic flow
inferred← citeshttps://doi.org/10.1007/s13369-025-10006-2openalex-snapshot
Aerodynamic Analysis and Geometric Optimization of Diversion Grooves in Blunt-Nose Corrected Projectiles
inferred← citeshttps://doi.org/10.1007/s42401-026-00449-2openalex-snapshot
Optimization and comparative study of drag and heat reduction via spiked jets in hypersonic flows
inferred← citeshttps://doi.org/10.1016/b978-0-323-91770-4.00003-3openalex-snapshot
Fluidic techniques
inferred← citeshttps://doi.org/10.1016/j.actaastro.2017.11.001openalex-snapshot
Investigation of drag and heat reduction induced by a novel combinational lateral jet and spike concept in supersonic flows based on conjugate heat transfer approach
inferred← citeshttps://doi.org/10.1016/j.actaastro.2018.11.052openalex-snapshot
Thermal protection characteristics for a combinational opposing jet and platelet transpiration cooling nose-tip
inferred← citeshttps://doi.org/10.1016/j.actaastro.2018.12.012openalex-snapshot
Design exploration of combinational spike and opposing jet concept in hypersonic flows based on CFD calculation and surrogate model
inferred← citeshttps://doi.org/10.1016/j.actaastro.2019.01.049openalex-snapshot
Performance assessment of energy deposition based drag reduction technique for Earth and Mars flight conditions
inferred← citeshttps://doi.org/10.1016/j.actaastro.2019.03.042openalex-snapshot
Aeroheating reduction for blunt body using aerodome jet
inferred← citeshttps://doi.org/10.1016/j.actaastro.2019.09.014openalex-snapshot
Hypersonic nonequilibrium flow simulations of a hemispherical nose with a counterflowing jet
inferred← citeshttps://doi.org/10.1016/j.actaastro.2019.10.045openalex-snapshot
Uncertainty and sensitivity study on blunt body's drag and heat reduction with combination of spike and opposing jet
inferred← citeshttps://doi.org/10.1016/j.actaastro.2020.03.004openalex-snapshot
Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows
inferred← citeshttps://doi.org/10.1016/j.actaastro.2020.05.048openalex-snapshot
Transient numerical simulation of hemispherical cone with combined opposing jet in hypersonic flow
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.actaastro.2020.09.021openalex-snapshot
Effect of the axial cavity with an opposing high-pressure jet combination in a Mach 6 flow condition
inferred← citeshttps://doi.org/10.1016/j.actaastro.2021.05.022openalex-snapshot
Fluid-thermal coupled investigation on the combinational spike and opposing/lateral jet in hypersonic flows
inferred← citeshttps://doi.org/10.1016/j.actaastro.2021.10.021openalex-snapshot
Parametric research on drag reduction and thermal protection of blunt-body with opposing jets of forward convergent nozzle in supersonic flows
inferred← citeshttps://doi.org/10.1016/j.actaastro.2022.06.032openalex-snapshot
Drag and heat reduction mechanism induced by jet interaction over a reusable launch vehicle in hypersonic flows
inferred← citeshttps://doi.org/10.1016/j.actaastro.2023.12.058openalex-snapshot
Three-dimensional numerical study on reducing hypersonic blunt body drag and aeroheating with spike-aerodisk-bleed air channel
inferred← citeshttps://doi.org/10.1016/j.actaastro.2025.05.021openalex-snapshot
Study on the aerodynamic characteristics of reentry vehicles with multi-mode combined drag and heat reduction devices
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2025.128058openalex-snapshot
Experimental investigation on mixing and thermal protection of jet cooling and transpiration cooling for rudder leading edge
inferred← citeshttps://doi.org/10.1016/j.ast.2018.03.051openalex-snapshot
Drag and heat reduction efficiency research on opposing jet in supersonic flows
inferred← citeshttps://doi.org/10.1016/j.ast.2018.11.021openalex-snapshot
Investigation on cooling effect with a combinational opposing jet and platelet transpiration concept 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.2019.105580openalex-snapshot
Study on the combined effect of various injection conditions on the drag reduction by a counter-flow jet in supersonic flow
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.ast.2020.105933openalex-snapshot
Mechanism study on drag reduction and thermal protection for the porous opposing jet in hypersonic flow
inferred← citeshttps://doi.org/10.1016/j.ast.2020.106065openalex-snapshot
Drag reduction analysis of counterflow jets in a short penetration mode
inferred← citeshttps://doi.org/10.1016/j.ast.2021.107064openalex-snapshot
Investigation on the drag reduction and thermal protection properties of the porous opposing jet in the supersonic flow: A parametric study with constant mass flow rate
inferred← citeshttps://doi.org/10.1016/j.ast.2021.107194openalex-snapshot
Heat and drag reduction of single and combined opposing jets in hypersonic nonequilibrium flows
inferred← citeshttps://doi.org/10.1016/j.ast.2022.107458openalex-snapshot
Theoretical and numerical analysis of pressure waves and aerodynamic characteristics in Hyperloop system under cracked-tube conditions
inferred← citeshttps://doi.org/10.1016/j.ast.2022.107507openalex-snapshot
Establishment process of spiked lateral jet in hypersonic flows
inferred← citeshttps://doi.org/10.1016/j.ast.2022.107603openalex-snapshot
Mechanism and prediction of flow oscillation based on counter-flow jet for drag reduction in hypersonic flow
inferred← citeshttps://doi.org/10.1016/j.ast.2022.107941openalex-snapshot
Behaviors of the long penetration mode with a hot counterflowing jet
inferred← citeshttps://doi.org/10.1016/j.ast.2025.110894openalex-snapshot
Flow behaviors of long penetration mode in rarefied hypersonic flow: Role of oblique-flow jet
inferred← citeshttps://doi.org/10.1016/j.ast.2025.111069openalex-snapshot
Characterization of drag and heat reduction of microporous jets for aerospace aircraft
inferred← citeshttps://doi.org/10.1016/j.biosystemseng.2024.01.012openalex-snapshot
Boundary modelling of the effective suction domain of an air-suction seed-metering device for quasi-spherical seeds
inferred← citeshttps://doi.org/10.1016/j.cja.2020.11.006openalex-snapshot
Preliminary study on heat flux measurement data of TT-0 flight test
inferred← citeshttps://doi.org/10.1016/j.csite.2023.102714openalex-snapshot
Study on hypersonic drag and heat reduction of a spiked blunt body with multiple flat aerodisks and rear opposing jets
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.icheatmasstransfer.2025.109910openalex-snapshot
A preliminary study of drag reduction mechanism via the aerospike-jet composite approach in low-altitude high-speed flow regimes
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2026.110706openalex-snapshot
Investigation of drag force and heat flux reduction coefficient on opposing jet
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2018.05.013openalex-snapshot
Detailed parametric investigations on drag and heat flux reduction induced by a combinational spike and opposing jet concept in hypersonic flows
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2018.06.154openalex-snapshot
Numerical investigation of blunt body’s heating load reduction with combination of spike and opposing jet
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2018.11.119openalex-snapshot
Coupled investigation on drag reduction and thermal protection mechanism induced by a novel combinational spike and multi-jet strategy in hypersonic flows
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2019.04.057openalex-snapshot
Insulating and absorbing heat of transpiration in a combinational opposing jet and platelet transpiration blunt body for hypersonic vehicle
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2020.120466openalex-snapshot
Thermal protection performance of a low pressure short penetration mode in opposing jet and its application
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.paerosci.2018.12.001openalex-snapshot
Drag and heat flux reduction mechanism induced by the spike and its combinations in supersonic flows: A review
inferred← citeshttps://doi.org/10.1016/j.paerosci.2019.100585openalex-snapshot
Forebody shock control devices for drag and aero-heating reduction: A comprehensive survey with a practical perspective
inferred← citeshttps://doi.org/10.1016/j.paerosci.2025.101093openalex-snapshot
Thermal protection and drag reduction induced by flow control devices in supersonic/hypersonic flows: A review
inferred← citeshttps://doi.org/10.1017/aer.2020.4openalex-snapshot
Influences of lateral jet location and its number on the drag reduction of a blunted body in supersonic flows
inferred← citeshttps://doi.org/10.1017/aer.2023.35openalex-snapshot
Investigation on the opposing jet penetration mode transition mechanism in the hypersonic flow
inferred← citeshttps://doi.org/10.1017/aer.2024.27openalex-snapshot
Aerothermal and aerodynamic characteristics of reusable hypersonic vehicles with heat transfer minimised sweepback
inferred← citeshttps://doi.org/10.1061/(asce)as.1943-5525.0000966openalex-snapshot
Novel Combinational Aerodisk and Lateral Jet Concept for Drag and Heat Reduction in Hypersonic Flows
inferred← citeshttps://doi.org/10.1061/(asce)as.1943-5525.0001467openalex-snapshot
Numerical Investigation on Flow Control of a Hypersonic Airfoil by Plasma Synthetic Jet
inferred← citeshttps://doi.org/10.1061/(asce)as.1943-5525.0001497openalex-snapshot
Unsteady Behavior of Long-Penetration Mode with a Counterflowing Jet
inferred← citeshttps://doi.org/10.1063/1.5119528openalex-snapshot
Numerical study of heat flux reduction mechanism of the counterflowing jet in rarefied flows
inferred← citeshttps://doi.org/10.1063/5.0124608openalex-snapshot
Coupled fluid–thermal analysis of the reduction mechanism for the drag and heat flux induced by jet interaction in a hypersonic reusable launch vehicle
inferred← citeshttps://doi.org/10.1063/5.0188137openalex-snapshot
Numerical investigation of effect of the design parameters of the counter-flow jet for drag reduction in hypersonic low-Reynolds number regime
inferred← citeshttps://doi.org/10.1063/5.0273810openalex-snapshot
Effect of induced magnetic field on magnetohydrodynamic control for high-velocity atmospheric entry
inferred← citeshttps://doi.org/10.1063/5.0274362openalex-snapshot
Numerical research and experiment on the thermal protection characteristics of opposing jets for rudder leading edge
inferred← citeshttps://doi.org/10.1063/5.0318539openalex-snapshot
Numerical investigation of aerodynamic performance and drag reduction in blunt bodies with aerodisk-mounted spikes under supersonic and hypersonic flow conditions
inferred← citeshttps://doi.org/10.1063/5.0343534openalex-snapshot
Numerical determination of the critical angle of attack for opposing-jet thermal-protection failure over a supersonic blunt body
inferred← citeshttps://doi.org/10.1088/1742-6596/1276/1/012031openalex-snapshot
Numerical analysis of slotted aerospike for drag reduction
inferred← citeshttps://doi.org/10.1109/ibcast61650.2024.10876962openalex-snapshot
Flight Mechanics of a Supersonic Projectile: A Parametric Investigation
inferred← citeshttps://doi.org/10.1109/icmae52228.2021.9522459openalex-snapshot
Numerical Study on Combined Thermal Protection System on Hypersonic Vehicle and Structure Parameters Influence of Acoustic Cavity
inferred← citeshttps://doi.org/10.1155/2018/7432961openalex-snapshot
Hypersonic Flow Field Reconfiguration and Drag Reduction of Blunt Body with Spikes and Sideward Jets
inferred← citeshttps://doi.org/10.1155/2021/5592855openalex-snapshot
Modeling and Analysis of Shock Reduction through Counterflow Plasma Jets
inferred← citeshttps://doi.org/10.1177/09544100211069796openalex-snapshot
Review of wave drag reduction techniques: Advances in active, passive, and hybrid flow control
inferred← citeshttps://doi.org/10.20910/jase.2020.14.4.18openalex-snapshot
Drag Reduction Effect by Counter-flow Jet on Conventional Rocket Configuration in Supersonic/Hypersonic Flow
inferred← citeshttps://doi.org/10.2514/1.j065183openalex-snapshot
Establishment of Long Penetration Mode in Rarefied Hypersonic Flow Utilizing Counter-/Oblique-Flow Jet
inferred← citeshttps://doi.org/10.2514/6.2021-2489openalex-snapshot
Large Eddy Simulation (LES) of Aerospike Nozzle assisted Supersonic Retro-Propulsion (SRP)
inferred← citeshttps://doi.org/10.2514/6.2022-1302openalex-snapshot
Flight Mechanics of a Supersonic Projectile: A Parametric Investigation
inferred← citeshttps://doi.org/10.2514/6.2023-2116openalex-snapshot
Shock Reduction through Multiple Opposing Jets in Atmospheric Entry Vehicle
inferred← citeshttps://doi.org/10.3390/aerospace12040308openalex-snapshot
Aerodynamic Characteristics of the Opposing Jet Combined with Magnetohydrodynamic Control in Hypersonic Nonequilibrium Flows
inferred← citeshttps://doi.org/10.3390/aerospace9120800openalex-snapshot
Geometric Optimization of Blunt Bodies with Aerodisk and Opposing Jet for Wave Drag and Heat Reduction
inferred← citeshttps://doi.org/10.3390/app10010180openalex-snapshot
Shock Reduction through Opposing Jets—Aerodynamic Performance and Flight Stability Perspectives
Editorial review for independent work. ICSAC — the Institute for Complexity
Science and Advanced Computing — runs a structured editorial panel for researchers
publishing outside journals, and publishes on CiteStamp rails. Submission is free
and goes through ORCID: icsacinstitute.org/submit.