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Sharp Leading Edge at Hypersonic Flight: Modeling and Flight Measurement

https://doi.org/10.2514/1.a32892
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What this work says

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

inferredcites →https://doi.org/10.1002/9781118932995.ch32openalex-snapshot
C/C‐SiC Materials Based on Melt Infiltration ‐ Manufacturing Methods and Experiences from Serial Production
inferredcites →https://doi.org/10.1016/b978-0-12-395737-5.50001-9openalex-snapshot
Progress in ASTRONAUTICS and AERONAUTICS
inferredcites →https://doi.org/10.1016/j.compstruct.2009.07.002openalex-snapshot
Secure tightening of a CMC fastener for the heat shield of re-entry vehicles
inferredcites →https://doi.org/10.1080/19942060.2008.11015212openalex-snapshot
Aero- and Thermodynamic Analysis of Shefex I
inferredcites →https://doi.org/10.2514/1.47172openalex-snapshot
Heat Balance of a Transpiration-Cooled Heat Shield
inferredcites →https://doi.org/10.2514/1.a33144openalex-snapshot
Transpiration-Cooled Hypersonic Flight Experiment: Setup, Flight Measurement, and Reconstruction
inferredcites →https://doi.org/10.2514/6.2006-7921openalex-snapshot
The SHEFEX Flight Experiment - Pathfinder Experiment for a Sky Based Test Facility

What points at this work

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

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Heated wind-tunnel experiments and numerical investigations onhypersonic blunt cone aerodynamic heating
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Effect of test parameter matching methods in a combustion-heated hypersonic wind tunnel on the aerothermal environment of a blunt cone
inferred← citeshttps://doi.org/10.1016/j.apsusc.2024.159812openalex-snapshot
Influence of Gas-Surface and Gas-Gas interactions on the energy accommodation coefficient in non-equilibrium hypersonic gas flows
inferred← citeshttps://doi.org/10.1016/j.ast.2024.109895openalex-snapshot
Main flight data on transpiration cooled sharp edge fins in hypersonic conditions on the sounding rocket HIFLIER
inferred← citeshttps://doi.org/10.1016/j.ast.2026.112514openalex-snapshot
Assessment of the mass flow rate of air in a shock-tunnel direct-connect scramjet combustor
inferred← citeshttps://doi.org/10.1016/j.compositesa.2018.03.008openalex-snapshot
Characterisation of electrical resistance for CMC materials up to 2000 K
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2023.106812openalex-snapshot
A Markov chain Monte Carlo analysis of carbon-phenolic ablation through a lumped physical model
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2023.106955openalex-snapshot
Application of the Markov chain Monte Carlo analysis through a lumped model in ablation test results of ablative and reradiative materials
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2024.126262openalex-snapshot
Research progress on transpiration cooling technology in force-thermal concentrated environments
inferred← citeshttps://doi.org/10.1061/(asce)as.1943-5525.0001042openalex-snapshot
One-Dimensional Aerodynamic Heating and Ablation Prediction
inferred← citeshttps://doi.org/10.1063/5.0017661openalex-snapshot
Role of chemical reactions in the stagnation point heat flux of rarefied hypersonic cylinder flows
inferred← citeshttps://doi.org/10.1080/09243046.2025.2488582openalex-snapshot
Dynamic modeling of ceramic matrix composite materials/metal bolted connection structure: considering the nonuniform microstructure effects on the connection interface based on macro-micro integrated model and parameter identification
inferred← citeshttps://doi.org/10.1155/2019/9754739openalex-snapshot
Hot Structure Flight Data of a Faceted Atmospheric Reentry Thermal Protection System
inferred← citeshttps://doi.org/10.2514/1.a33144openalex-snapshot
Transpiration-Cooled Hypersonic Flight Experiment: Setup, Flight Measurement, and Reconstruction
inferred← citeshttps://doi.org/10.2514/1.a36748openalex-snapshot
Long Duration Hypersonic Flight Experiment ATHEAt
inferred← citeshttps://doi.org/10.2514/1.j055298openalex-snapshot
Flowfield and Pressure Decay Analysis of Porous Cones
inferred← citeshttps://doi.org/10.2514/1.t4950openalex-snapshot
Hypersonic Aeroheating Characteristics of Leading Edges with Different Nose Radii
inferred← citeshttps://doi.org/10.2514/1.t7248openalex-snapshot
Design Principles for Transpiration-Cooled Ceramic Sharp Leading Edges
inferred← citeshttps://doi.org/10.2514/6.2015-3661openalex-snapshot
Characterization of the Flow Field of Anisotropic Porous Cones with Different Wall Thickness
inferred← citeshttps://doi.org/10.2514/6.2016-4428openalex-snapshot
Aerodynamic Heating Prediction Tool for a Supersonic Vehicle for Conceptual Design Phase
inferred← citeshttps://doi.org/10.2514/6.2017-2362openalex-snapshot
Thermal Response of an Ablator: Model and Time Resolved Imaging
inferred← citeshttps://doi.org/10.2514/6.2021-1519openalex-snapshot
Geometry Dependence of Transpiration Cooling for Hypersonic Systems
inferred← citeshttps://doi.org/10.2514/6.2023-0437openalex-snapshot
Aerodynamic Effects and Heat Flux Augmentation of a Transpiration Cooled Hypersonic Sharp Leading Edge
inferred← citeshttps://doi.org/10.2514/6.2024-2384openalex-snapshot
Shock Wave Boundary Layer Interaction on the STORT Flight Experiment
inferred← citeshttps://doi.org/10.2514/6.2026-0528openalex-snapshot
Long Duration Hypersonic Flight Experiment ATHEAt
inferred← citeshttps://doi.org/10.3390/aerospace13030278openalex-snapshot
Thermo-Mechanical Design of the C/C-SiC-Based Thermal Protection Structure for the Forebody of the Hypersonic Sounding Rocket STORT
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