[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Erickson, 1979 - Google Patents

Effect of Spanwise Blowing on the Aerodynamic Characteristics of the F-5E

Erickson, 1979

Document ID
3703671308988039299
Author
Erickson G
Publication year
Publication venue
Journal of aircraft

External Links

Snippet

STABLE leading-edge vortices are characteristic of the flow over thin, highly sweptback wings at moderate-tohigh angles of attack. This flow situation is illustrated in the water- tunnel photograph in Fig. 1 and occurs because the favorable spanwise pressure gradient …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction
    • Y02T50/16Drag reduction by influencing airflow
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02Aircraft characterised by the type or position of power plant
    • B64D27/16Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air-flow over aircraft surfaces, not otherwise provided for
    • B64C23/06Influencing air-flow over aircraft surfaces, not otherwise provided for by generating vortices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/10Shape of wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/10All-wing aircraft
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GASES [GHG] EMISSION, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C21/00Influencing air-flow over aircraft surfaces by affecting boundary-layer flow

Similar Documents

Publication Publication Date Title
Lefebvre et al. Design of high wing loading compact electric airplane utilizing co-flow jet flow control
Erickson Water-tunnel studies of leading-edge vortices
Céron-Muñoz et al. Experimental investigation of wing-tip devices on the reduction of induced drag
Jones Reduction of wave drag by antisymmetric arrangement of wings and bodies.
Braslow A review of factors affecting boundary-layer transition
Carter et al. Blended-wing-body transonic aerodynamics: summary of ground tests and sample results
Gall et al. Aerodynamic characteristics of biplanes with winglets
Erickson Effect of Spanwise Blowing on the Aerodynamic Characteristics of the F-5E
Alford et al. An Exploratory Investigation of the Low-Speed Aerodynamic Characteristics of Variable-Wing-Sweep Airplane Configurations
Penland et al. An aerodynamic analysis of several hypersonic research airplane concepts from M= 0.2 to 6.0
Pezzella et al. Aerodynamic performance analysis of a winged re-entry vehicle from hypersonic down to subsonic speed
Thibert et al. A review of ONERA aerodynamic research in support of a future supersonic transport aircraft
Axelson Investigation of a slat in several different positions on an NACA 64A010 airfoil for a wide range of subsonic Mach numbers
Bykerk et al. Longitudinal And Lateral-Directional Aerodynamics of a Re-Usable High-Speed Vehicle
Seginer et al. Augmentation of fighter-aircraft performance by spanwise blowing over the wing leading edge
Polhamus et al. Configuration aerodynamics
Banchy et al. Crossflow Attenuated Natural Laminar Flow (CATNLF) Technology Development: From Concept to Flight
Wagner et al. Supersonic laminar flow control on commercial transports
Rao et al. Analysis on Aerodynamic Performance of Single-skinned Parawing in the Hypersonic Rarefied flow
Erickson et al. Augmentation of maneuver performance by spanwise blowing
Fetterman et al. A review of hypersonic cruise vehicles
Mann et al. A Foward-Swept-Wing Fighter Configuration Designed by a Transonic Computational Method
Lei et al. Enhancing Supersonic Rudder Control Surface Using Co-flow Jet Active Flow Control
Rich F-12 series aircraft aerodynamic and thermodynamic design in retrospect
Lei et al. Control Surfaces for Supersonic Airfoil Using Co-flow Jet Active Flow Control