Soudakov et al., 2018 - Google Patents
Investigations of active and passive flow control on civil aircraft with high-lift configurationSoudakov et al., 2018
View PDF- Document ID
- 8733662667882650819
- Author
- Soudakov V
- Voevodin A
- Mamonova E
- Publication year
- Publication venue
- AIP Conference Proceedings
External Links
Snippet
A high-lift configuration of the civil aircraft including body, wing in high-lift configuration, nacelle and pylon is considered in the present work. Numerical simulations of the flow have been carried out in the framework of Reynolds averaged Navier-Stokes (RANS) equations …
- 238000007664 blowing 0 abstract description 15
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
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
- B64C3/14—Aerofoil profile
-
- 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
- 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
- B64C1/0009—Aerodynamic aspects
-
- 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
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
-
- 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
-
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air-flow over aircraft surfaces by affecting boundary-layer flow
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GASES [GHG] EMISSION, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
-
- 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
-
- 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
- Y02T70/00—Maritime or waterways transport
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Jang et al. | Numerical investigation of an airfoil with a Gurney flap | |
US20090230251A1 (en) | Airplane engine pylon comprising at least one protruding element to generate a vortex of the airflow | |
US6942178B2 (en) | Mach weighted area ruling for supersonic vehicles | |
Larkin et al. | A design analysis of vertical stabilisers for Blended Wing Body aircraft | |
Prince et al. | Aerodynamic stall suppression on aerofoil sections using passive air-jet vortex generators | |
Dakka Dr et al. | Aerodynamic design and exploration of a blended wing body aircraft at subsonic speed | |
Jin et al. | Computational analysis of the aerodynamic performance of a long-endurance UAV | |
US20160272335A1 (en) | Nose cone structure for pylon of aircraft with wing-hung layout | |
Iannelli et al. | Design of a high-lift system for a laminar wing | |
Yang et al. | Effects of design parameters on longitudinal static stability for WIG craft | |
Nouri et al. | Numerical investigation of aerodynamic characteristics of NACA 23018 airfoil with a gurney flap | |
Radespiel et al. | Fundamentals in coanda flap design | |
Pavlenko et al. | Concept of medium twin-engine STOL transport airplane | |
Edi et al. | Civil-transport wing design concept exploiting new technologies | |
US7311287B2 (en) | Methods for incorporating area ruled surfaces in a supersonic aircraft | |
Soudakov et al. | Investigations of active and passive flow control on civil aircraft with high-lift configuration | |
Bohannon | Passive flow control on civil aircraft flaps using sub-boundary layer vortex generators in the AWIATOR programme | |
Raj Mohamed et al. | Bio-inspired optimization of leading edge slat | |
US20050116107A1 (en) | Area ruling for vertical stabilizers | |
Voevodin et al. | Control of flow past a model aircraft in the landing configuration using aerodynamic strakes | |
Mamonova et al. | Vortex flow on the wing of aircraft and flow control to improve lift properties | |
Kafyeke et al. | Development of high-lift systems for the Bombardier CRJ-700 | |
Qin et al. | Aerodynamics of a multi-element airfoil near ground | |
Popov et al. | Improving aircraft fuel efficiency by using the adaptive wing and winglets | |
Lei | Flow simulation of an supersonic transport configuration at low-speed and high-lift conditions |