Shi, 2014 - Google Patents
Performance estimation for fluidic thrust vectoring nozzle coupled with aero-engineShi, 2014
- Document ID
- 9898709749508047924
- Author
- Shi J
- Publication year
- Publication venue
- 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
External Links
Snippet
HE demand of multi-functional propulsion exhausting system will be heightened with the development of efficient combat characteristic for the future aircraft, eg thrust vectoring control, stealth ability et. al.. To fulfill these demands, the mechanical controlling system of …
- 238000000605 extraction 0 abstract description 43
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
-
- 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
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/14—Technologies for the improvement of mechanical efficiency of a conventional ICE
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
- F02K7/16—Composite ram-jet/turbo-jet engines
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Waithe et al. | An experimental and computational investigation of multiple injection ports in a convergent-divergent nozzle for fluidic thrust vectoring | |
Gorton et al. | Active flow control on a boundary-layer-ingesting inlet | |
Deng et al. | Numerical simulation of fluidic thrust vectoring in an axisymmetric supersonic nozzle | |
Kim et al. | Flow simulation of N2B hybrid wing body configuration | |
Ma et al. | Mathematical modeling and characteristic analysis for over-under turbine based combined cycle engine | |
CN105446167B (en) | Hypersonic scramjet engine real-time model, emulation mode | |
Lv et al. | Numerical investigation of improving the performance of a single expansion ramp nozzle at off-design conditions by secondary injection | |
Deere et al. | Computational study of an axisymmetric dual throat fluidic thrust vectoring nozzle for a supersonic aircraft application | |
Shi | Performance estimation for fluidic thrust vectoring nozzle coupled with aero-engine | |
Ali et al. | Combination of fluidic thrust modulation and vectoring in a 2D nozzle | |
Huang et al. | Design and experimental study of a bypass dual throat nozzle with the ability of short/vertical takeoff and landing | |
Arend et al. | Generation after next propulsor research: Robust design for embedded engine systems | |
Sun et al. | Influences of geometric parameters on serpentine nozzles for turbofan | |
Jingwei et al. | Numerical investigation on a new concept of shock vector control nozzle | |
Shi et al. | Investigation on flow characteristics of SVC nozzles | |
Wu et al. | Visualization and analysis on the thrust vectoring control in three-dimensional dual-throat nozzles | |
Du et al. | Investigation on the supplementary combustion scheme for the divergent section of a solid rocket engine nozzle | |
Salimi et al. | Computational investigation of effects of sideinjection geometry on thrust-vectoring performance in a fuel-injected dual throat nozzle | |
Lin et al. | Effective boundary conditions and numerical method for flow characteristics of aeroengine compressor at high Mach flight | |
Frohnapfel et al. | Fan rotor flow measurements in a turbofan engine operating with inlet swirl distortion | |
Akman | Subsonic-transonic submerged intake design for a cruise missile | |
Xiaolin et al. | Performance estimation for serpentine nozzle coupled with aero-engine | |
Song et al. | Investigation on flow characteristics and parameters optimization of a new concept of TC nozzle | |
Shi et al. | Investigation on flow characteristics and performance estimation of a hybrid SVC nozzle | |
Shi et al. | Numerical Investigation on Flow Fields of SVC Nozzle with Bypass Injection |