On the public citation graph

Effect of a spike on the drag and on the aerodynamic stability of blunt bodies in supersonic flow

0 signed · 35 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.
Claim with ORCID
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 See whether every reference in this work resolves to a known work and none has been retracted — and get a dated CiteStamped badge you can embed.
See reference health

What this work says

Outgoing claims: the papers this work cites, builds on, or argues with.

inferredcites →https://doi.org/10.1080/14786440708520987openalex-snapshot
LXVIII. Experiments on separation of boundary layers on probes in front of blunt-nosed bodies in a supersonic air stream
inferredcites →https://doi.org/10.2514/3.2255openalex-snapshot
A flow-separation spike for hypersonic control of a hemisphere-cylinder
inferredcites →https://doi.org/10.2514/3.29195openalex-snapshot
Regarding the utility of spiked blunt bodies.
inferredcites →https://doi.org/10.2514/8.7945openalex-snapshot
Preliminary Investigations of Spiked Bodies at Hypersonic Speeds

What points at this work

Incoming claims: where this work appears in other papers’ reference lists and arguments.

inferred← citeshttps://doi.org/10.2139/ssrn.4201874openalex-extracted
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/s42496-023-00180-7openalex-snapshot
Determining Dynamic Stability of a Re-entry Capsule at Free Fall
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.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.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.icheatmasstransfer.2026.110996openalex-snapshot
Experimental and numerical investigations of the flow control mechanism with combined spike-porous jet techniques in hypersonic flow
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.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/s0045-7930(97)00011-xopenalex-snapshot
Navier-Stokes solution for a heat shield with and without a forward facing spike
inferred← citeshttps://doi.org/10.1017/s0001924000002554openalex-snapshot
Experimental investigation on spiked body in hypersonic flow
inferred← citeshttps://doi.org/10.1017/s0001924000017085openalex-snapshot
Forward facing spike effects on bodies of different cross section in supersonic flow
inferred← citeshttps://doi.org/10.1108/aeat-04-2023-0088openalex-snapshot
Aero-spike and aero-disk effects of on wave drag reduction of supersonic flow past over blunt body
inferred← citeshttps://doi.org/10.1134/s0015462825601779openalex-snapshot
Recent Developments in Unsteady Flow Characteristics over Spiked Blunt Bodies: A Survey
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/10.1260/1759-3107.1.2.93openalex-snapshot
Experimental Investigation of the Effects of Aerospike Geometry on Aerodynamic Drag and Heat Transfer Rates for a Blunt Body Configuration at Hypersonic Mach Numbers
inferred← citeshttps://doi.org/10.1615/computthermalscien.2022043279openalex-snapshot
AEROTHERMODYNAMICS OF COMBINED SPIKE AND COUNTERFLOW JET TECHNIQUE FOR REACTING HYPERSONIC FLOWS
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/10.2514/2.6910openalex-snapshot
Flowfield Around Spike-Tipped Bodies for High Attack Angles at Mach 4.5
inferred← citeshttps://doi.org/10.2514/3.25920openalex-snapshot
Aerodynamic effects of probe-induced flow separation on bluff bodiesat transonic Mach numbers
inferred← citeshttps://doi.org/10.2514/6.1985-103openalex-snapshot
Aerodynamic effects of probe-induced flow separation of bluff bodiesat transonic Mach numbers
inferred← citeshttps://doi.org/10.2514/6.2000-268openalex-snapshot
Reduction of the wave drag of a blunt body by means of a standoff spike
inferred← citeshttps://doi.org/10.2514/6.2001-1828openalex-snapshot
Thermal protection and drag reduction with use of spike in hypersonic flow
inferred← citeshttps://doi.org/10.2514/6.2001-2464openalex-snapshot
Flow field around spike-tipped bodies
inferred← citeshttps://doi.org/10.2514/6.2001-888openalex-snapshot
Blunt body wave drag reduction by means of a standoff spike
inferred← citeshttps://doi.org/10.2514/6.2002-2918openalex-snapshot
High-Pressure Shock Tunnel Experiments and CFD Calculations on Spike-Tipped Blunt Bodies
inferred← citeshttps://doi.org/10.2514/6.2004-2428openalex-snapshot
Some Aerodynamic and Aerothermodynamic Considerations for Reusable Launch Vehicles
inferred← citeshttps://doi.org/10.2514/6.2015-2109openalex-snapshot
Supersonic Tests of the Double Gap Disk-Gap Band Parachute and Fluid Structure Interaction Simulation
inferred← citeshttps://doi.org/10.61653/joast.v65i4.2013.872openalex-snapshot
Drag Reduction of a Hemispherical Body Adopting Spike at Supersonic Speed
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.