GRODSKY et al. - Google Patents
A simulation study of landing of a typical medium L/D entry vehicleGRODSKY et al.
- Document ID
- 12017000720461338732
- Author
- GRODSKY M
- MANDOUR J
- Publication venue
- Control and Flight Dynamics Conference
External Links
Snippet
Propulsion systems selected for commercial transports must provide efficient and reliable performance over a broad range of conditions. These air-planes are used over both short and long route segments, on non-standard days, and at a range of altitudes to meet airline …
- 238000004088 simulation 0 title 1
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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/30—Control parameters, e.g. input parameters
-
- 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 |
---|---|---|
EP1942259B2 (en) | Operating line control of a compression system with flow recirculation | |
Spang III et al. | Control of jet engines | |
CA2910833C (en) | Secondary nozzle for jet engine | |
EP2177735A2 (en) | Turbofan | |
US11378017B2 (en) | Supersonic aircraft turbofan | |
Vdoviak et al. | VCE test bed engine for supersonic cruise research | |
GRODSKY et al. | A simulation study of landing of a typical medium L/D entry vehicle | |
Taylor | Inlet duct-engine exhaust nozzle airflow matching for the supersonic transport | |
Mahmood et al. | Thrust reverser for a mixed exhaust high bypass ratio turbofan engine and its effect on aircraft and engine performance | |
US3387457A (en) | Combined turbojet and turboprop engine | |
Lieblein | A review of lift fan propulsion systems for civil VTOL transports | |
Hines | Variable stream control engine for supersonic propulsion | |
CHAMPAGNE | Jet noise reduction concepts for the supersonic transport | |
FRANCISCUS | Turbine bypass engine-A new supersonic cruise propulsion concept | |
Kerler et al. | Experimental Investigation of an Engine Quick-Start System with Compact Air Supply for Rotorcraft Application | |
Lieblein | Problem areas for lift fan propulsion for civil VTOL transports | |
COX | Performance investigation of variable turbine geometry in gas turbine engines | |
Kepler et al. | Performance potential of air turbo-ramjet employing supersonic through-flow fan | |
Beheim et al. | Subsonic and supersonic propulsion | |
Zellner et al. | Integration of turbo-expander and turbo-ramjet engines in hypersonic vehicles | |
Gertsma et al. | Propulsion system for research VTOL transports | |
Bagby et al. | Effect of turbofan cycle variables on aircraft cruise performance. | |
Brimelow | Performance Matching of the Propulsion System | |
KUTNEY | AEROTHERMODYNAMIC CONSIDERATIONS OF THE TIP TURBINE DRIVEN LIFT/CRUISE FAN PROPULSION SYSTEM | |
JPS61283755A (en) | Gas turbine engine for aircraft |