On the public citation graph

Aerodynamic Optimization of Hypersonic Blunted Waveriders Considering Payload Constraint

0 signed · 34 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 See whether every reference in this work resolves to a known work and none has been retracted — and get a dated CiteStamped badge you can embed.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/10.1007/bf00532683openalex-snapshot
A method for designing lifting configurations for high supersonic speeds, using axisymmetric flow fields
inferredcites →https://doi.org/10.1016/0160-9327(79)90054-1openalex-snapshot
The aerodynamic design of aircraft
inferredcites →https://doi.org/10.1016/j.ast.2015.01.025openalex-snapshot
Novel approach for design of a waverider vehicle generated from axisymmetric supersonic flows past a pointed von Karman ogive
inferredcites →https://doi.org/10.1016/j.ast.2015.04.015openalex-snapshot
Effect of elastic deformation on the trajectory of aerial separation
inferredcites →https://doi.org/10.1016/j.ast.2017.09.010openalex-snapshot
A design approach of wide-speed-range vehicles based on the cone-derived theory
inferredcites →https://doi.org/10.1016/j.ast.2017.12.020openalex-snapshot
Modification of hypersonic waveriders by vorticity-based boundary layer displacement thickness determination method
inferredcites →https://doi.org/10.1016/j.ast.2019.01.029openalex-snapshot
Planform-customized waverider design integrating with vortex effect
inferredcites →https://doi.org/10.1016/j.ast.2020.106266openalex-snapshot
Integration of inward-turning inlet with airframe based on dual-waverider concept
inferredcites →https://doi.org/10.1016/j.ast.2023.108801openalex-snapshot
Aerodynamic optimization of hypersonic blunted waveriders based on symbolic regression
inferredcites →https://doi.org/10.1016/j.paerosci.2020.100606openalex-snapshot
An overview of research on wide-speed range waverider configuration
inferredcites →https://doi.org/10.1017/s0368393100071662openalex-snapshot
Aerodynamic Problems of Manned Space Vehicles
inferredcites →https://doi.org/10.1177/09544100211029454openalex-snapshot
Effect of upper surface shape on waverider performances
inferredcites →https://doi.org/10.2514/1.20079openalex-snapshot
Optimization of Viscous Waveriders Derived from Axisymmetric Power-Law Blunt Body Flows
inferredcites →https://doi.org/10.2514/1.29958openalex-snapshot
Universal Parametric Geometry Representation Method
inferredcites →https://doi.org/10.2514/1.a33253openalex-snapshot
Multidisciplinary Design Optimization of Waverider-Derived Crew Reentry Vehicles
inferredcites →https://doi.org/10.2514/1.c032340openalex-snapshot
Parametric Geometry Model for Design Studies of Tailless Supersonic Aircraft
inferredcites →https://doi.org/10.2514/1.j053458openalex-snapshot
Experimental Investigation of a Mach 3.5 Waverider Designed Using Computational Fluid Dynamics
inferredcites →https://doi.org/10.2514/1.j059087openalex-snapshot
Design and Optimization Method for Hypersonic Quasi-Waverider
inferredcites →https://doi.org/10.2514/1.j059904openalex-snapshot
Parametric Study on Lateral–Directional Stability of Hypersonic Waverider
inferredcites →https://doi.org/10.2514/3.26451openalex-snapshot
Hypersonic waverider test vehicle - A logical next step
inferredcites →https://doi.org/10.2514/3.46438openalex-snapshot
Design tradeoffs on scramjet engine integrated hypersonic waverider vehicles
inferredcites →https://doi.org/10.2514/3.46848openalex-snapshot
Wedge-cone waverider configuration for engine-airframe interaction
inferredcites →https://doi.org/10.2514/3.5084openalex-snapshot
A class of three-dimensional, optimum hypersonic wings.
inferredcites →https://doi.org/10.2514/3.522openalex-snapshot
Reference temperature method and Reynolds analogy for chemically reacting nonequilibrium flowfields
inferredcites →https://doi.org/10.2514/4.861956openalex-snapshot
Hypersonic and High-Temperature Gas Dynamics, Second Edition
inferredcites →https://doi.org/10.2514/5.9781600862342.0051.0080openalex-snapshot
Hypersonic Aerodynamics
inferredcites →https://doi.org/10.2514/6.1987-272openalex-snapshot
Viscous optimized hypersonic waveriders
inferredcites →https://doi.org/10.2514/6.1988-369openalex-snapshot
Viscous optimized hypersonic waveriders designed from axisymmetric flow fields
inferredcites →https://doi.org/10.2514/6.1992-302openalex-snapshot
Hypersonic waveriders - Effects of chemically reacting flow and viscous interaction
inferredcites →https://doi.org/10.2514/6.1992-308openalex-snapshot
A hypersonic waverider test vehicle - The logical next step
inferredcites →https://doi.org/10.2514/6.1994-380openalex-snapshot
Waverider configurations based on non-axisymmetric flow fields for engine-airframe integration
inferredcites →https://doi.org/10.2514/6.2001-1834openalex-snapshot
Stability and control analysis of a Wave-Rider TSTO second stage
inferredcites →https://doi.org/10.2514/6.2001-1849openalex-snapshot
Design and analysis of payload-optimized waveriders
inferredcites →https://doi.org/10.2514/6.2005-511openalex-snapshot
The Osculating Flowfield Method of Waverider Geometry Generation
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.