Schatzman et al., 2017 - Google Patents
Time-varying loads of co-axial rotor blade crossingsSchatzman et al., 2017
View PDF- Document ID
- 13669489711353833382
- Author
- Schatzman N
- Komerath N
- Romander E
- Publication year
- Publication venue
- SAE International Journal of Aerospace
External Links
Snippet
The blade crossing event of a coaxial counter-rotating rotor is a potential source of noise and impulsive blade loads. Blade crossings occur many times during each rotor revolution. In previous research by the authors, this phenomenon was analyzed by simulating two …
- 238000004088 simulation 0 abstract description 55
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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies
- Y02T50/67—Relevant aircraft propulsion technologies
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/80—Technologies aiming to reduce green house gasses emissions common to all road transportation technologies
- Y02T10/82—Tools or systems for aerodynamic design
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Tinoco et al. | Summary data from the sixth AIAA CFD drag prediction workshop: CRM cases | |
Nielsen et al. | High-performance aerodynamic computations for aerospace applications | |
Nichols | Addition of a local correlation-based boundary layer transition model to the CREATETM-AV Kestrel unstructured flow solver | |
Sheridan et al. | Evaluation of vspaero analysis capabilities for conceptual design of aircraft with propeller-blown wings | |
Ortun et al. | In-plane airloads of a propeller with inflow angle: prediction vs. experiment | |
Schatzman et al. | Time-varying loads of co-axial rotor blade crossings | |
Bellocq et al. | Multidisciplinary Assessment of the Control of the Propellers of a Pusher Geared Open Rotor—Part I: Zero-Dimensional Performance Model for Counter-Rotating Propellers | |
Smith et al. | Reduction of aft fuselage drag on the C-130 using microvanes | |
Hayami et al. | Numerical investigation of aerodynamic interference on coaxial rotor | |
Holst et al. | Current Status of the Finite-Element Fluid Solver (COFFE) within HPCMP CREATE™-AV Kestrel | |
Rivers et al. | Computational Fluid Dynamics Analyses for the High-Lift Common Research Model Using the USM3D and FUN3D Flow Solvers | |
Linton et al. | An actuator surface method for ship-helicopter dynamic interface simulations | |
Sethunathan et al. | Analysis of aerodynamic characteristics of a supercritical airfoil for low speed aircraft | |
Radespiel et al. | Simulation of wing stall | |
Noelting et al. | The Lattice-Boltzmann method: an alternative to LES for complex aerodynamic and aeroacoustic simulations in the aerospace industry | |
Qiao et al. | Numerical simulation of distributed propulsion systems using CFD | |
Schatzman et al. | Modeling Shed Vorticity from Coaxial Blade Interactions | |
Samal et al. | Reduction of wingtip vortex from suction at wingtip | |
Jia et al. | Assessment of turbulence modeling and wake-grid resolution for lift-offset coaxial rotor simulations | |
Stuermer et al. | Aerodynamic and aeroacoustic analysis of contra-rotating open rotor propulsion systems at low-speed flight conditions | |
Abdol-Hamid et al. | DPW-6 Results Using FUN3D With Focus on k-kL-MEAH2015 Turbulence Model | |
Bornhoft et al. | Large-eddy simulations of the CRM65 swept wing under real and artificial icing conditions | |
Xu | CFD investigation into propeller spacing and pitch angle for a ducted twin counter rotating propeller system | |
Şahbaz et al. | Numerical and experimental investigation of rotor aerodynamics in ground effect with inclined planes | |
Şahbaz | Aerodynamic investigation of a model scale helicopter rotor in ground effect |