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

Neubauer et al., 2023 - Google Patents

Introduction of an Online Ice Accretion Database

Neubauer et al., 2023

Document ID
9845893141862423495
Author
Neubauer T
Puffing R
Publication year
Publication venue
SAE International Journal of Advances and Current Practices in Mobility

External Links

Snippet

In the course of the Horizon 2020 project ICE GENESIS of the European Union, an experimental database was developed to host documentation of icing experiments. The database serves as a source of information for numerical code development and validation …
Continue reading at www.sae.org (other versions)

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5009Computer-aided design using simulation
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies

Similar Documents

Publication Publication Date Title
Potapczuk Aircraft icing research at NASA Glenn research center
US20120109585A1 (en) Method and System to Account for Angle of Attack Effects in Engine Noise Shielding Tests
Robinson et al. Aspects of aero-engine nacelle drag
Goodwin et al. Turbofan ice crystal rollback investigation and preparations leading to inaugural ice crystal engine test at NASA PSL-3 test facility
Isikveren Quasi-analytical modelling and optimisation techniques for transport aircraft design
Woodard et al. Summary of ice shape geometric fidelity studies on an iced swept wing
Chai et al. Tradeoff study between cost and environmental impact of aircraft using simultaneous optimization of airframe and engine cycle
Neubauer et al. Introduction of an Online Ice Accretion Database
Hoheisel et al. The influence of engine thrust behaviour on the aerodynamics of engine airframe integration
Filippone et al. Flyover noise measurements and predictions of commercial airplanes
Atasoy et al. Enhanced cruise range prediction for narrow-body turbofan commercial aircraft based on QAR data
Knoth et al. Flow analysis of a helicopter engine side air intake
Tanaka et al. Icing on full-scale swept wings in flight and icing wind tunnel
Chen et al. Numerical analysis of rotor aero-acoustic characteristics for ice detection
Ly et al. Evaluation of the aerodynamic performance of the counter rotating turbo fan COBRA by means of experimental and numerical data
Şahin et al. An approach to estimate aircraft fuel consumption for the descent phase
Huang et al. Aircraft Departure Fuel Consumption Improvement Model Based On Flight Data
Tsao et al. Further Evaluation of Scaling Methods for Rotorcraft Icing
Reasor Jr et al. Numerical predictions of static-pressure-error corrections for a modified T-38C aircraft
Luber et al. The impact of dynamic loads on the design of military aircraft
Mack et al. Determination of extrapolation distance with measured pressure signatures from two low-boom models
Davis et al. A proposal for integration of wind tunnel and engine test programs for the evaluation of airframe-propulsion compatibility using numerical simulations
Kreeger et al. Collaborative experiments and computations in aircraft icing
Del Mônaco Monteiro et al. In-flight thrust determination for high-bypass-ratio turbofan using residual error methodology
Kinaschuk Development of method of testing a set of screen-exhaust devices in the helicopter Mi-8MSB-B