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

Ericsson et al., 1999 - Google Patents

Effect of nose slenderness on forebody flow control

Ericsson et al., 1999

Document ID
13008097558541684347
Author
Ericsson L
Beyers M
Publication year
Publication venue
Journal of aircraft

External Links

Snippet

Background In Ref. 2 the pneumatic vortex control (PVC) devices were investigated on a 6% scale model of the F-16 forebody. The tests were performed at 0·®· 18 deg, MD 0: 8, and Re D 0: 85£ 106 based on the maximum forebody cross-section dimension (Fig. 1). An …
Continue reading at arc.aiaa.org (other versions)

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
    • 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
    • Y02T50/162—Wing tip vortex reduction
    • Y02T50/164—Winglets
    • 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
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • 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
    • B64C21/00—Influencing air-flow over aircraft surfaces by affecting boundary-layer flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for

Similar Documents

Publication Publication Date Title
Pamadi Performance, stability, dynamics, and control of airplanes
Ericsson Sources of high alpha vortex asymmetry at zero sideslip
Ericsson et al. Steady and unsteady vortex-induced asymmetric loads on slender vehicles
Hitzel et al. Vortex flow aerodynamic challenges in the design space for future fighter aircraft
ERICSSON et al. Analysis of flow separation effects on the dynamics of a large space booster
Ericsson et al. Alleviation of vortex-induced asymmetric loads
Alcorn et al. The X-31 experience-aerodynamic impediments to post-stall agility
Ericsson et al. Effect of nose slenderness on forebody flow control
Renals et al. NATO AVT-350 Task Group: Comparison of Experimental and CFD Results of Forebody Blowing on the Bristol-ICE Model
Madani et al. Investigating the effect of the placement of the split drag rudder control system along the wing span of a flying wing aircraft on rolling and yawing moments.
Golubev et al. Control of separated and vortex flow using perforated aircraft surface
Liu et al. Aerodynamics
Nielsen Missile aerodynamics-past, present, future
Ericsson et al. Forebody flow control at conditions of naturally occurring separation asymmetry
Ericsson et al. Fluid mechanics considerations for successful design of forebody flow control
Wickenheiser et al. Evaluation of bio-inspired morphing concepts with regard to aircraft dynamics and performance
Sattarov et al. Aerodynamic performance improvement of UAV by means of leading-edge vortex generators
Miao et al. The Aerodynamic Characteristics of a Diamond Joined‐Wing Morphing Aircraft
Yang et al. Numerical investigation of unsteady aerodynamic characteristics of a pitching missile
Ericsson Reflections regarding recent rotary rig results
Seginer et al. Magnus effects on spinning transonic finned missiles
Wang et al. The design of jet vane of thrust vector control system
Ya Numerical simulation of dynamic deployment of the folding wing
Ericsson et al. Conceptual fluid/motion coupling in the Herbst supermaneuver
JAMES, JR Aerodynamics of rocket plume interactions at supersonic speeds