RETTIE, 1980 - Google Patents
Theoretical and Experimental studies of aerodynamic interference effects(aerodynamic forces on winglets and on wing nacelle configurations for the YC-14 and KC …RETTIE, 1980
- Document ID
- 10830541038052574301
- Author
- RETTIE I
- Publication year
- Publication venue
- 1980. 19
External Links
- 230000000694 effects 0 title description 2
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
- Y02T50/60—Efficient propulsion technologies
- Y02T50/67—Relevant aircraft propulsion technologies
-
- 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
-
- 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
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically
- B64C29/0008—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically
- B64C29/0008—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded
- B64C29/0041—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
- B64C29/005—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors the motors being fixed relative to the fuselage
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4917332A (en) | Wingtip vortex turbine | |
US4629147A (en) | Over-the-wing propeller | |
RETTIE | Theoretical and Experimental studies of aerodynamic interference effects(aerodynamic forces on winglets and on wing nacelle configurations for the YC-14 and KC-135 aircraft) | |
Driggers | Study of aerodynamic technology for VSTOL fighter/attack aircraft, phase 1[Final Report, Nov. 1977- May 1978] | |
SU1826436A1 (en) | Aircraft power plant | |
Whitcomb | Methods for reducing subsonic drag due to lift | |
US3465990A (en) | Aircraft having energy-conserving means | |
GB1071075A (en) | Improvements in aircraft | |
Arndt | Propfans go full scale | |
Sedgwick | Investigation of non-symmetric two-dimensional nozzles installed in twin-engine tactical aircraft | |
Nangia | Aspects of forward swept wing research at the University of Bristol | |
Rettie | Theoretical and Experimental studies of aerodynamic interference effects | |
RAO et al. | Wind-tunnel studies of advanced cargo aircraft concepts(leading edge vortex flaps for drag reduction)[Final Report, 22 Jun. 1979- 21 Jun. 1980] | |
RU2005661C1 (en) | Ground-effect apparatus | |
JOHNSON | Over-the-wing propeller(Patent) | |
BANGERT et al. | Effects of Nacelle configuration/position on performance of subsonic transport[Final Report] | |
WILSON, III et al. | CTOL, STOVL, and VTOL fighter design comparisons | |
Patterson Jr | Wingtip vortex turbine | |
WESOKY et al. | Wind tunnel tests of a 20 inch diameter 1. 15 pressure ratio fan engine model(Aerodynamic wind tunnel performance of high bypass pressure ratio fan engine for STOL aircraft) | |
Boles et al. | Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft | |
MARK | Study of aerodynamic technology for single-cruise-engine V/STOL fighter/attack aircraft[Final Report, Jun. 1981- Feb. 1982] | |
TICE et al. | A study of altitude-constrained supersonic cruise transport concepts | |
GARLAND et al. | Phase 2 and 3 wind tunnel tests of the J-97 powered, external augmentor V/STOL model(at Ames 40 by 80 wind tunnel) | |
MAITA et al. | Powered lift aerodynamics of USB STOL aircraft(Upper Surface Blowing) | |
SOLOMON | A study of the lift-to-drag ratio capability of caret wing waveriders[M. S. Thesis Interim Scientific Report] |