Zhu et al., 2021 - Google Patents
Fluid–structure interaction-based aerodynamic modeling for flight dynamics simulation of parafoil systemZhu et al., 2021
- Document ID
- 6499626783330770190
- Author
- Zhu H
- Sun Q
- Liu X
- Liu J
- Sun H
- Wu W
- Tan P
- Chen Z
- Publication year
- Publication venue
- Nonlinear Dynamics
External Links
Snippet
Prediction of aerodynamic force is a crucial issue for parafoil canopy as the strong nonlinear fluid–structure interaction (FSI) between the flexible canopy material and flow field. Flight tests and wind tunnel experiments are difficult to analyze the aerodynamics of parafoil …
- 238000004088 simulation 0 title abstract description 34
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
- G06F17/50—Computer-aided design
- G06F17/5086—Mechanical design, e.g. parametric or variational design
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
- B64C1/06—Frames; Stringers; Longerons; Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air-flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air-flow over aircraft surfaces, not otherwise provided for by generating vortices
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F2217/00—Indexing scheme relating to computer aided design [CAD]
- G06F2217/16—Numerical modeling
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Zhu et al. | Fluid–structure interaction-based aerodynamic modeling for flight dynamics simulation of parafoil system | |
Yousefi et al. | Three-dimensional suction flow control and suction jet length optimization of NACA 0012 wing | |
Ghoreyshi et al. | Prediction of aerodynamic characteristics of ram-air parachutes | |
Piedra et al. | Computational aerodynamics analysis of a light sport aircraft: Compliance study for stall speed and longitudinal stability certification requirements | |
Ghoreyshi et al. | Computational aerodynamic modeling for flight dynamics simulation of ram-air parachutes | |
Tao et al. | Computational fluid dynamics based dynamic modeling of parafoil system | |
Ahuja et al. | Three-dimensional viscous coupling & flow separation enhancements to an inviscid surface vorticity flow solver | |
Guimarães et al. | Flexibility Assessment of the Aeroelastic-flight-dynamic Behavior for Supersonic Aircraft | |
Dimitriadis et al. | Aerodynamic stability derivative calculations using the compressible source and doublet panel method | |
Dimitriadis et al. | Prediction of aerodynamic loads and stability derivatives using the unsteady Source and Doublet Panel Method for preliminary aircraft design | |
Bergeron et al. | Near-body/Cartesian off-body simulations for C-17 and extraction parachute | |
Smith et al. | The validation of an airfoil in the ground effect regime using 2-D CFD analysis | |
Soneda et al. | Multi-fidelity aeroelastic simulation of a morphing wing trailing edge | |
Flores et al. | Simple and efficient numerical tools for the analysis of parachutes | |
An | Aeroelastic design of a lightweight distributed electric propulsion aircraft with flutter and strength requirements | |
Ghoreyshi et al. | CFD calculation of stability and control derivatives for ram-air parachutes | |
Zhu et al. | Aerodynamic prediction for flight dynamics simulation of parafoil system and airdrop test validation | |
Niksch et al. | Six degree-of-freedom dynamical model of a morphing aircraft | |
Sedlacek et al. | Numerical investigations of vortex formation on a generic multiple-swept-wing configuration | |
Rhodes et al. | Roughness receptivity in swept-wing boundary layers–computations | |
Hosangadi et al. | Improved stall prediction for swept wings using low-order aerodynamics | |
Pfnür et al. | Yaw-control efficiency analysis for a diamond wing configuration with outboard split flaps | |
Ananda et al. | Stall/post-stall modeling of the longitudinal characteristics of a general aviation aircraft | |
Todorov | Determination of the aerodynamic characteristics of a light aircraft using ANSYS workbench and FLUENT software | |
Niksch et al. | Morphing Aircaft Dynamical Model: Longitudinal Shape Changes |