Nothing Special   »   [go: up one dir, main page]

Moushegian, 2024 - Google Patents

Fast High-Fidelity Analysis of a Hovering Rotor with a Dual-Solver Hybrid CFD Methodology in HCPMP CREATE-AV Helios

Moushegian, 2024

Document ID
14837171760138978167
Author
Moushegian A
Publication year
Publication venue
AIAA SCITECH 2024 Forum

External Links

Snippet

Detailed aerodynamic analysis of rotorcraft with unsteady Reynolds-Averaged Navier- Stokes (uRANS) solvers strains the computational resources of even the most well-funded programs, driven by small time step and large computational grid requirements to …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06F—ELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50—Computer-aided design
    • G06F17/5009—Computer-aided design using simulation
    • G06F17/5018—Computer-aided design using simulation using finite difference methods or finite element methods
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06F—ELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/20—Handling natural language data
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06F—ELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/10—Complex mathematical operations

Similar Documents

Publication Publication Date Title
Hu et al. Hovering efficiency optimization of the ducted propeller with weight penalty taken into account
Goulos et al. Mission performance simulation of integrated helicopter–engine systems using an aeroelastic rotor model
Lee et al. Review of vortex methods for rotor aerodynamics and wake dynamics
Costes et al. Rotorcraft simulations: a challenge for CFD
McDaniel et al. The HPCMP CREATETM-AV Kestrel Computational Environment and its Relation to NASA’s CFD Vision 2030
Ahmad et al. Estimation of stability parameters for wide body aircraft using computational techniques
Perullo et al. Effects of advanced engine technology on open rotor cycle selection and performance
Lim Application of parametric airfoil design for rotor performance improvement
Wissink et al. Overview of new capabilities in helios version 9.0
Wilbur et al. UH-60A rotor analysis with an accurate dual-formulation hybrid aeroelastic methodology
Pfeiffer et al. Implementation of a heterogeneous, variable-fidelity framework for flight mechanics analysis in preliminary aircraft design
Lopes ANOPP2’s Farassat Formulations Internal Functional Module (AFFIFM) Reference Manual
Solano et al. Parametric Structural Weight Estimation for the PEGASUS Concept Considering Dynamic Aeroelastic Effects
Ciampa et al. Preliminary design for flexible aircraft in a collaborative environment
Moushegian Fast High-Fidelity Analysis of a Hovering Rotor with a Dual-Solver Hybrid CFD Methodology in HCPMP CREATE-AV Helios
Jain Computational fluid dynamics transition models validation for rotors in unsteady flow conditions
Johnson et al. Rotorcraft conceptual design environment
Pfeiffer et al. Aircraft configuration analysis using a low-fidelity, physics based aerospace framework under uncertainty considerations
Koning et al. Mid-Fidelity Computational Fluid Dynamics Analysis of the Elytron 4S UAV Concept
Liu Multi-fidelity Optimization of Ducted Fan for eVTOL Aircraft
Omran et al. Global aircraft aero-propulsive linear parameter-varying model using design of experiments
Stratton Empirical modeling of tilt-rotor aerodynamic performance
Eshcol et al. A comparative study of two hover prediction methodologies
Avera et al. OpenMDAO/NDARC framework for assessing performance impact of rotor technology integration
Schatzman et al. Time-varying loads of co-axial rotor blade crossings