Seginer et al., 1986 - Google Patents
Performance augmentation of a 60-degree delta aircraft configurationby spanwise blowingSeginer et al., 1986
- Document ID
- 9442190224066505
- Author
- Seginer A
- Salomon M
- Publication year
- Publication venue
- Journal of Aircraft
External Links
Snippet
MOST existing and next-generation advanced tactical fighter aircraft and air-to-air missiles make extensive use of nonlinear vortex lift. 1 The phenomenon of the formation of the leading-edge vortices and of the additional lift they induce has been well understood for the …
- 238000007664 blowing 0 title description 28
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
- B64C3/10—Shape of wings
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air-flow over aircraft surfaces by affecting boundary-layer flow
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US10661884B2 (en) | Oblique blended wing body aircraft | |
Stanewsky | Adaptive wing and flow control technology | |
US6578798B1 (en) | Airlifting surface division | |
Polhamus | Applying slender wing benefits to military aircraft | |
Djojodihardjo et al. | Research, development and recent patents on aerodynamic surface circulation control-A critical review | |
Jones | The oblique wing—aircraft design for transonic and low supersonic speeds | |
Seginer et al. | Performance augmentation of a 60-degree delta aircraft configurationby spanwise blowing | |
Murri et al. | Actuated forebody strake controls for the F-18 high-alpha research vehicle | |
Levin et al. | Self-induced roll oscillations of low-aspect-ratio rectangular wings | |
ERICSSON | Control of forebody flow asymmetry-A critical review | |
Wood | Vortex flows at supersonic speeds | |
Udartsev et al. | Effect of Leading Edge Volumic Shape Vortex Generators on Static Hysteresis of Unmanned Aerial Vehicle Wing | |
Erickson | Effect of Spanwise Blowing on the Aerodynamic Characteristics of the F-5E | |
KRAMER et al. | Forebody vortex control with jet and slot blowing on an F/A-18 | |
Seginer et al. | Augmentation of fighter-aircraft performance by spanwise blowing over the wing leading edge | |
Reddy | Spanwise pressure distribution on delta wing with leading-edge vortex flap | |
Li et al. | Trade-off of lifting and propulsion capacity of tandem flapping-fixed airfoils by inclining the stroke plane | |
Moeller et al. | Hingeless flow control over a Delta-wing planform | |
Ericsson et al. | Effect of nose slenderness on forebody flow control | |
Min et al. | Modeling and autopilot design of blended wing-body UAV | |
Rao et al. | Analysis on Aerodynamic Performance of Single-skinned Parawing in the Hypersonic Rarefied flow | |
Freeman Jr et al. | Impact of far-aft center of gravity for a single-stage-to-orbit vehicle | |
Reddy | Effect of leading-edge vortex flaps on aerodynamic performance of delta wings | |
Gibson et al. | Natural laminar flow wing concept for supersonic transports | |
Rameshbhai et al. | Enhancing the Performance of Aerofoil Using Novel Injection–Suction Method |