Guegan et al., 2011 - Google Patents
Experimental investigation of the kinematics of post-impact ice fragmentsGuegan et al., 2011
View PDF- Document ID
- 1853021279735136119
- Author
- Guegan P
- Othman R
- Lebreton D
- Pasco F
- Villedieu P
- Meyssonnier J
- Wintenberger S
- Publication year
- Publication venue
- International journal of impact engineering
External Links
Snippet
Hail is more hazardous for aircraft engines compared to rain and snow, mainly, because of its solid nature and high water content. In extreme cases it can lead to engine flame out. In order to avoid such situations, aero engines should be designed to withstand hail ingestion …
- 238000009114 investigational therapy 0 title description 5
Classifications
-
- 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
- Y02T50/671—Measures to reduce the propulsor weight
- Y02T50/672—Measures to reduce the propulsor weight using composites
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Guegan et al. | Experimental investigation of the kinematics of post-impact ice fragments | |
| Kim et al. | Experimental investigation of high velocity ice impacts on woven carbon/epoxy composite panels | |
| Gohardani | Impact of erosion testing aspects on current and future flight conditions | |
| Zhou et al. | Experimental and numerical investigation of high velocity soft impact loading on aircraft materials | |
| Yang et al. | Review of damage mechanism and protection of aero-engine blades based on impact properties | |
| Chanetz et al. | Experimental Aerodynamics | |
| Wright et al. | Mixed phase modeling in GlennICE with application to engine icing | |
| Hauk et al. | Investigation of the impact behaviour of ice particles | |
| Jingyu et al. | Numerical simulation of a UAV impacting engine fan blades | |
| Flegel | Ice Crystal Icing Research at NASA Glenn Research Center | |
| Woods et al. | Hyper-X stage separation wind-tunnel test program | |
| Vargas et al. | Ice particle impacts on a moving wedge | |
| Mata-Díaz et al. | Experimental analysis of high velocity impacts of composite fragments | |
| Pan et al. | Impact characteristics of hailstones simulating ingestion by turbofan aeroengines | |
| D'Souza et al. | Experimental validation of a UAS at engine ingestion conditions: Part I Experiments | |
| Reagle et al. | Study of microparticle rebound characteristics under high temperature conditions | |
| Yang et al. | Experimental investigation of an ice particle impinging on a flat plate | |
| Fei et al. | Aerodynamic characteristics of store during lateral jet assisted separation from cavity using free drop technique | |
| Zhang et al. | Application of numerical methods for crashworthiness investigation of a large aircraft wing impact with a tree | |
| Feulner et al. | Ice crystal ingestion in a turbofan engine | |
| Zheng et al. | Aerodynamics and bird ingestion characteristics of a bulge-adjustable turboprop engine inlet | |
| Hu et al. | Breakup and collision of water droplet for mass injection pre-compression cooling | |
| Holden et al. | Reviews of Studies of Boundary Layer Transition in Hypersonic Flows over Axisymmetric and Elliptic Cones Conducted in the CUBRC Shock Tunnels | |
| Moffat et al. | Prediction of bird impact pressures and damage using MSC/DYTRAN | |
| Jun et al. | Damage sensitivity of a wing-type leading edge structure impacted by a bird |