Enkelmann et al., 2020 - Google Patents
Comparison of a physical model and a machine learning approach for a more accurate assessment of fuel efficiency measuresEnkelmann et al., 2020
View PDF- Document ID
- 13986347905359665304
- Author
- Enkelmann F
- Heigl R
- Pfingsten K
- Publication year
- Publication venue
- AIAA Scitech 2020 Forum
External Links
Snippet
The paper focuses on a more accurate quantification method of fuel efficiency measures which can be applied to commercial transport airplanes. These measures or modifications can for example affect the engine or aerodynamical efficiency. Full flight data of a …
- 239000000446 fuel 0 title abstract description 69
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
-
- 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
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Cole et al. | Higher-order free-wake method for propeller–wing systems | |
RU2599108C1 (en) | Method of monitoring loads and accumulated fatigue damage in operating conditions of aircraft | |
Jelicic et al. | Online monitoring of aircraft modal parameters during flight test based on permanent output-only modal analysis | |
Krajček et al. | Aircraft performance monitoring from flight data | |
Baumann et al. | Evaluation of the aircraft fuel economy using advanced statistics and machine learning | |
Kenyon et al. | Wake dynamics and rotor‐fuselage aerodynamic interactions | |
Kilic et al. | Digital twin for Electronic Centralized Aircraft Monitoring by machine learning algorithms | |
Neves et al. | Unsteady aerodynamics analysis and modelling of a Slingsby Firefly aircraft: Detached-Eddy Simulation model and flight test validation | |
Renaud et al. | Numerical analysis of hub and fuselage drag breakdown of a helicopter configuration | |
Noll et al. | Impact of active controls technology on structural integrity | |
Enkelmann et al. | Comparison of a physical model and a machine learning approach for a more accurate assessment of fuel efficiency measures | |
Hall | CFD modeling of US army UAVs using NASA's OVERFLOW CFD code | |
CN108333945A (en) | The distributed fully excitation input signal design method of airplane flutter experiment | |
Laurence III et al. | Development and flight test results of a small UAS distributed flush airdata system | |
Reveles et al. | Rotor/propeller model fidelity effects on propeller-wing interactional aerodynamics | |
Kayran | Flight flutter testing and aeroelastic stability of aircraft | |
Deo et al. | Flight performance monitoring with optimal filtering applications | |
Van der Ven et al. | A modelling framework for the calculation of structural loads for fatigue life prediction of helicopter airframe components | |
Sinske et al. | HALO flight test with instrumented under-wing stores for aeroelastic and load measurements in the DLR project iLOADS | |
US12002306B2 (en) | Systems and methods for assessing aircraft performance, aircraft fuel efficiencies, and aircraft fuel reduction technologies | |
Schatzman et al. | Time-varying loads of co-axial rotor blade crossings | |
Li et al. | Uncertainty quantification analysis with arbitrary polynomial chaos method: Application in slipstream effect of propeller aircraft | |
Liu et al. | Assessment of potential benefit of formation flight at preliminary aircraft design level | |
Buck et al. | Aircraft acceleration prediction due to atmospheric disturbances with flight data validation | |
Radha Krishnan et al. | Comparative Study and Aerodynamic Analysis of Rectangular Wing Using High‐Lift Systems |