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Numerical analysis of pressure oscillations over axisymmetric spiked blunt bodies at Mach 6.80
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What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.1007/978-3-0348-8243-9_5openalex-snapshot
Numerical Methods for Compressible Flow
inferredcites →https://doi.org/10.1007/978-3-642-85952-6openalex-snapshot
Computational Methods for Fluid Flow
inferredcites →https://doi.org/10.1007/bfb0019784openalex-snapshot
Numerical solution of the unsteady navier-stokes equations for the oscillatory flow over a concave body
inferredcites →https://doi.org/10.1007/s002310000091openalex-snapshot
Peak heating for reattachment of separated flow on a spiked blunt-body
inferredcites →https://doi.org/10.1016/s0376-0421(00)00005-1openalex-snapshot
Elements of computational fluid dynamics on block structured grids using implicit solvers
inferredcites →https://doi.org/10.1017/s0022112062000427openalex-snapshot
Hypersonic flow over spiked cones
inferredcites →https://doi.org/10.2514/3.57160openalex-snapshot
Unsteady Aerodynamic Considerations in the Design of a Drag-Reduction Spike
inferredcites →https://doi.org/10.2514/3.8893openalex-snapshot
Modes of shock-wave oscillations on spike-tipped bodies
inferredcites →https://doi.org/10.2514/6.1980-62openalex-snapshot
Flow oscillations of spike-tipped bodies
inferredcites →https://doi.org/10.2514/6.1993-887openalex-snapshot
Numerical investigation of supersonic flows around a spiked blunt-body
inferredcites →https://doi.org/10.2514/6.1995-48openalex-snapshot
Multigrid unsteady Navier-Stokes calculations with aeroelastic applications
What points at this work
Incoming claims: where this work appears in other papers’ reference lists and arguments.
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Design Optimization and Aerothermodynamic Analysis Over a Supersonic Vehicle
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/s00348-020-03130-2openalex-snapshot
Shock-related unsteadiness of axisymmetric spiked bodies in supersonic flow
inferred← citeshttps://doi.org/10.1007/s42401-025-00431-4openalex-snapshot
Mathematical modelling and development methods for high-speed flow control over spiked blunt bodies: a review
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.2014.02.009openalex-snapshot
The drag reduction in spherical spiked blunt body
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.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.2011.06.001openalex-snapshot
Recent advances in the aerothermodynamics of spiked hypersonic vehicles
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.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/s0001924000003675openalex-snapshot
Numerical simulation of the flow field over conical, disc and flat spiked body at Mach 6
inferred← citeshttps://doi.org/10.1017/s0001924000009052openalex-snapshot
Investigation of flow asymmetry around axi-symmetric spiked blunt bodies in hypersonic speeds
inferred← citeshttps://doi.org/10.1017/s0022112009006235openalex-snapshot
High-speed unsteady flows around spiked-blunt bodies
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/10.1063/5.0075583openalex-snapshot
Unsteady pulsating flowfield over spiked axisymmetric forebody at hypersonic 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/10.1063/5.0262232openalex-snapshot
Drag reduction in high-speed flow over a spherical bluff body with a disk-ended spike
inferred← citeshttps://doi.org/10.1142/s0217984920503704openalex-snapshot
Numerical exploration on drag and heat reduction mechanism of a spike-tipped supersonic blunt nose
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/10.1177/09544100221140942openalex-snapshot
Supersonic flow investigation of a drag reducing conical spike on a hemispherically blunted nose body
inferred← citeshttps://doi.org/10.12989/aas.2020.7.4.371openalex-snapshot
Drag reduction for payload fairing of satellite launch vehicle with aerospike in transonic and low supersonic speeds
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/10.2514/1.46655openalex-snapshot
Drag Reduction Using Aerodisks for Hypersonic Hemispherical Bodies
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.a34250openalex-snapshot
Control of Aerodynamic Drag and Heating of Nose Cones Through Taper Spikes
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.j059369openalex-snapshot
Parametric Experimental Studies on Supersonic Flow Unsteadiness over a Hemispherical Spiked Body
inferred← citeshttps://doi.org/10.2514/6.2008-4707openalex-snapshot
Aerospike for Drag Reduction in Hypersonic Flow
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/10.2514/6.2011-2228openalex-snapshot
Heat Transfer Analysis over Disc and Hemispherical Spike Attached to Blunt-Nosed Body at Mach 6
inferred← citeshttps://doi.org/10.2514/6.2019-2316openalex-snapshot
Effect of Body Nose Fairing on the Unsteady Flow Characteristics over Spiked Flat Faced Cylinder at Supersonic Speed
inferred← citeshttps://doi.org/10.3390/aerospace11030188openalex-snapshot
Experimental Investigation of the Shock-Related Unsteadiness around a Spiked-Blunt Body Based on a Novel DMD Energy Sorting Criterion
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/10.48550/arxiv.1912.13368openalex-snapshot
Parametric experimental studies on the shock related unsteadiness in a hemispherical spiked body at supersonic flow
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