Gubanova et al., 2014 - Google Patents
High-Lift System Design by Numerical Methods and Wind Tunnel VerificationGubanova et al., 2014
View PDF- Document ID
- 1627411301277812037
- Author
- Gubanova M
- Bragin N
- Perchenkov E
- Slitinskaya A
- Publication year
- Publication venue
- 29th Congress of the International Council of the Aeronautical Sciences
External Links
Snippet
The results of experimental investigations of a civil plane wing high-lift devices and its local aerodynamics are presented. The analysis of flow has been carried out by both force measurements at different Reynolds numbers and flow visualization using mini-tufts. New …
- 238000005457 optimization 0 abstract description 10
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
- Y02T50/10—Drag reduction
- Y02T50/16—Drag reduction by influencing airflow
- Y02T50/166—Drag reduction by influencing airflow by influencing the boundary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air-flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air-flow over aircraft surfaces, not otherwise provided for by generating vortices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/16—Aircraft characterised by the type or position of power plant of jet type
- B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/34—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members
- B64C9/36—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members the members being fuselages or nacelles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air-flow over aircraft surfaces by affecting boundary-layer flow
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/12—Boundary layer controls by using electromagnetic tiles, fluid ionizers, static charges or plasma
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Dehpanah et al. | The aerodynamic design evaluation of a blended-wing-body configuration | |
Elham et al. | Winglet multi-objective shape optimization | |
Ting et al. | Supersonic configurations at low speeds (SCALOS): Model geometry and aerodynamic results | |
Savoni et al. | Pylon design for a short range transport aircraft with over-the-wing mounted UHBR engines | |
Petrov | Aerodynamics of STOL airplanes with powered high-lift systems | |
Trancossi et al. | A new aircraft architecture based on the ACHEON Coanda effect nozzle: flight model and energy evaluation | |
Dakka Dr et al. | Aerodynamic design and exploration of a blended wing body aircraft at subsonic speed | |
Neigapula et al. | A study of high lift aerodynamic devices on commercial aircrafts | |
Baals et al. | Aerodynamic design integration of supersonic aircraft | |
Jin et al. | Computational analysis of the aerodynamic performance of a long-endurance UAV | |
Taleghani et al. | Numerical study of flow control to increase vertical tail effectiveness of an aircraft by tangential blowing | |
Zhao et al. | Investigation of propeller slipstream effects on lateral and directional static stability of transport aircraft | |
Machado et al. | Toward the Development of an Underwing Boundary Layer Ingesting Distributed Propulsion System for the SUSAN Electrofan | |
Becker et al. | Numerical aerodynamics in transport aircraft design | |
Bragin et al. | Improvement of aerodynamics of civil plane wing high-lift devices | |
Gubanova et al. | High-Lift System Design by Numerical Methods and Wind Tunnel Verification | |
Keller et al. | Investigation and improvement of directional stability and control of a propeller-driven stol aircraft | |
Sommerwerk et al. | Aeroelastic performance assessment of a wing with coanda effect circulation control via fluid-structure interaction | |
Popov et al. | Improving aircraft fuel efficiency by using the adaptive wing and winglets | |
Zuhair et al. | Trailing edge geometry effect on the aerodynamics of low-speed BWB aerial vehicles | |
Lei et al. | Experimental Optimization of Leading-Edge Deflection Angles for an SST Configuration at Low Speed | |
Chen et al. | Progress of blended-wing-body aircraft development at Northwestern Polytechnical University | |
Bragin et al. | On the influence of small-dimensional elements on the aerodynamics of supercritical wings | |
Petrov et al. | Experimental investigations of externally blown flap efficiency on the model of short takeoff and landing twin-engine transport aircraft | |
Palmer et al. | Effect of curved boundary layer fences on aerodynamic efficiency |