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Design and fabrication of a Mach 8 contoured nozzle for the LENS facility

https://doi.org/10.2514/6.1996-585
0 signed · 16 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.

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What this work says

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

inferredcites →https://doi.org/10.2514/3.26655openalex-snapshot
Flow quality of hypersonic wind-tunnel nozzles designed using computational fluid dynamics
inferredcites →https://doi.org/10.2514/3.30160openalex-snapshot
Aerodynamic design of axisymmetric hypersonic wind-tunnel nozzles
inferredcites →https://doi.org/10.2514/6.1992-4009openalex-snapshot
CAN-DO, CFD-based Aerodynamic Nozzle Design and Optimization programfor supersonic/hypersonic wind tunnels
inferredcites →https://doi.org/10.2514/6.1992-4010openalex-snapshot
A comparison of experimental data with CFD for the NSWC Hypervelocity Wind Tunnel No. 9 Mach 14 Nozzle
inferredcites →https://doi.org/10.2514/6.1995-291openalex-snapshot
Calibration, validation, and evaluation studies in the LENS facility

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.4148298openalex-extracted
inferred← citeshttps://doi.org/10.1016/j.addma.2022.103379openalex-snapshot
A Workflow for Designing Contoured Axisymmetric Nozzles for Enhancing Additively Manufactured Cold Spray Deposits
inferred← citeshttps://doi.org/10.1061/(asce)as.1943-5525.0001296openalex-snapshot
Toward a Low Noise Shock Tunnel Facility via Multiobjective Optimization of Hypersonic Nozzle
inferred← citeshttps://doi.org/10.1063/5.0159468openalex-snapshot
Hypervelocity imperfect gas nozzle design with shared wave-elimination contour
inferred← citeshttps://doi.org/10.2514/2.7565openalex-snapshot
Diode Laser Sensor for Velocity Measurements in Hypervelocity Flows
inferred← citeshttps://doi.org/10.2514/6.1997-3267openalex-snapshot
Tunable diode-laser absorption measurements of temperature, velocity, and H2O in hypervelocity flows
inferred← citeshttps://doi.org/10.2514/6.1998-2496openalex-snapshot
Design, fabrication, and calibration of a Mach 6.5 hypersonic shock tunnel nozzle for scramjet testing applications
inferred← citeshttps://doi.org/10.2514/6.1998-2699openalex-snapshot
Measurements of gas temperature and velocity in hypervelocity flows using diode-laser sensors
inferred← citeshttps://doi.org/10.2514/6.2000-677openalex-snapshot
Inviscid design of hypersonic wind tunnel nozzles for a real gas
inferred← citeshttps://doi.org/10.2514/6.2005-903openalex-snapshot
Numerical Evaluation of Flow Conditions in the LENS Reflected Shock-Tunnel Facilities
inferred← citeshttps://doi.org/10.7282/t3ng4qsbopenalex-snapshot
Analysis and design of quiet hypersonic wind tunnels
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