GB479598A - Improvements relating to the reduction of resistance of bodies moving in fluids - Google Patents
Improvements relating to the reduction of resistance of bodies moving in fluidsInfo
- Publication number
- GB479598A GB479598A GB18777/36A GB1877736A GB479598A GB 479598 A GB479598 A GB 479598A GB 18777/36 A GB18777/36 A GB 18777/36A GB 1877736 A GB1877736 A GB 1877736A GB 479598 A GB479598 A GB 479598A
- Authority
- GB
- United Kingdom
- Prior art keywords
- area
- air
- interstices
- ducts
- areas
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 239000012530 fluid Substances 0.000 title 1
- 238000010276 construction Methods 0.000 abstract 1
- 239000004744 fabric Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
- B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
- B64C21/06—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for sucking
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/04—Boundary layer controls by actively generating fluid flow
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/06—Boundary layer controls by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/20—Boundary layer controls by passively inducing fluid flow, e.g. by means of a pressure difference between both ends of a slot or duct
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/22—Boundary layer controls by using a surface having multiple apertures of relatively small openings other than slots
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
479,598. Reducing resistance of aircraft. MILES, F. G. July 6, 1936, Nos. 18777 and 21704. [Class 4] In an aeroplane in which the boundary layer of air can be sucked off an area or areas of its skin through ducts, the area or areas have by virtue of their nature or construction numerous small perforations or interstices spaced substantially uniformly over the area so as virtually to render the area uniformly porous to air. Perforations or interstices of the order of 420 per square inch are stated to be suitable to give the desired porosity. As shown, an aeroengine 3 drives a centrifugal blower 5 to suck air through the wing covering, ducts 7, 6 having guide vanes 8, and exhaust it above the fuselage. Passages are formed in the wing beneath the covering and are provided with valves 13 operable together or severally. According to the first Provisional Specification, porous fabric may be stretched over closely perforated sheetmetal.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB18777/36A GB479598A (en) | 1936-07-06 | 1936-07-06 | Improvements relating to the reduction of resistance of bodies moving in fluids |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB18777/36A GB479598A (en) | 1936-07-06 | 1936-07-06 | Improvements relating to the reduction of resistance of bodies moving in fluids |
Publications (1)
Publication Number | Publication Date |
---|---|
GB479598A true GB479598A (en) | 1938-02-07 |
Family
ID=10118233
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB18777/36A Expired GB479598A (en) | 1936-07-06 | 1936-07-06 | Improvements relating to the reduction of resistance of bodies moving in fluids |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB479598A (en) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2480036A (en) * | 1946-05-13 | 1949-08-23 | Armstrong Whitworth Co Eng | Airplane with boundary layer control and powered by internal combustion turbines |
US2488991A (en) * | 1943-06-25 | 1949-11-22 | Edward A Stalker | Boundary layer control for drag reduction |
US2508288A (en) * | 1944-12-08 | 1950-05-16 | Bristol Aeroplane Co Ltd | Gas turbine power plant for aircraft |
US2509890A (en) * | 1945-03-13 | 1950-05-30 | Edward A Stalker | Jet-propelled aircraft with boundary layer control |
US2605983A (en) * | 1946-04-06 | 1952-08-05 | Edward A Stalker | Gas turbine power plant and boundary layer control system for aircraft |
US2643832A (en) * | 1949-01-26 | 1953-06-30 | Imp Trust For The Encouragemen | Aerodynamic lift-producing device |
US2659552A (en) * | 1950-06-09 | 1953-11-17 | Edward A Stalker | Aircraft surface with boundary layer control |
US2686020A (en) * | 1951-03-16 | 1954-08-10 | Wandscheer John | Boundary layer control for aircraft |
US2745611A (en) * | 1946-05-29 | 1956-05-15 | Rateau Soc | Jet propulsion and boundary layer control system for aircraft |
US2751168A (en) * | 1949-05-05 | 1956-06-19 | Edward A Stalker | Boundary layer induction system for aircraft power plant |
US2833492A (en) * | 1955-02-07 | 1958-05-06 | Harlan D Fowler | Boundary layer control system with aerodynamic glove |
US2867391A (en) * | 1953-12-07 | 1959-01-06 | Jacobsen Edwin | Ducted wing for aircraft |
US2945644A (en) * | 1953-10-09 | 1960-07-19 | Lockheed Aircraft Corp | Wing structure incorporating boundary layer control |
US3054579A (en) * | 1957-03-14 | 1962-09-18 | Woldemar A Bary | Aircraft with slow speed landing and take-off |
US8286909B2 (en) | 2008-02-08 | 2012-10-16 | Stratocomm Corporation | Boundary layer propulsion airship with related system and method |
-
1936
- 1936-07-06 GB GB18777/36A patent/GB479598A/en not_active Expired
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2488991A (en) * | 1943-06-25 | 1949-11-22 | Edward A Stalker | Boundary layer control for drag reduction |
US2508288A (en) * | 1944-12-08 | 1950-05-16 | Bristol Aeroplane Co Ltd | Gas turbine power plant for aircraft |
US2509890A (en) * | 1945-03-13 | 1950-05-30 | Edward A Stalker | Jet-propelled aircraft with boundary layer control |
US2605983A (en) * | 1946-04-06 | 1952-08-05 | Edward A Stalker | Gas turbine power plant and boundary layer control system for aircraft |
US2480036A (en) * | 1946-05-13 | 1949-08-23 | Armstrong Whitworth Co Eng | Airplane with boundary layer control and powered by internal combustion turbines |
US2745611A (en) * | 1946-05-29 | 1956-05-15 | Rateau Soc | Jet propulsion and boundary layer control system for aircraft |
US2643832A (en) * | 1949-01-26 | 1953-06-30 | Imp Trust For The Encouragemen | Aerodynamic lift-producing device |
US2751168A (en) * | 1949-05-05 | 1956-06-19 | Edward A Stalker | Boundary layer induction system for aircraft power plant |
US2659552A (en) * | 1950-06-09 | 1953-11-17 | Edward A Stalker | Aircraft surface with boundary layer control |
US2686020A (en) * | 1951-03-16 | 1954-08-10 | Wandscheer John | Boundary layer control for aircraft |
US2945644A (en) * | 1953-10-09 | 1960-07-19 | Lockheed Aircraft Corp | Wing structure incorporating boundary layer control |
US2867391A (en) * | 1953-12-07 | 1959-01-06 | Jacobsen Edwin | Ducted wing for aircraft |
US2833492A (en) * | 1955-02-07 | 1958-05-06 | Harlan D Fowler | Boundary layer control system with aerodynamic glove |
US3054579A (en) * | 1957-03-14 | 1962-09-18 | Woldemar A Bary | Aircraft with slow speed landing and take-off |
US8286909B2 (en) | 2008-02-08 | 2012-10-16 | Stratocomm Corporation | Boundary layer propulsion airship with related system and method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB479598A (en) | Improvements relating to the reduction of resistance of bodies moving in fluids | |
US2833492A (en) | Boundary layer control system with aerodynamic glove | |
GB518663A (en) | Improvements in or relating to aircraft, hydroplanes and the like | |
US3584812A (en) | Aircraft lifting surfaces | |
GB718421A (en) | Improvements relating to boundary layer control means for aerofoils and other boundary walls | |
GB542878A (en) | Improvements in means for preventing ice accumulation on aerofoil and like surfaces | |
GB404817A (en) | Improvements in apparatus provided with dynamic lifting surfaces or with dynamic lifting-propelling surfaces, particularly aircraft | |
GB652942A (en) | Improvements in or relating to aircraft | |
DE590004C (en) | Process for influencing the circulation flow on areas of an aircraft that generate lift | |
GB713426A (en) | Improvements in or relating to external surfaces for moving craft | |
GB610622A (en) | Improvements in and relating to solid boundary surfaces for fluid streams | |
US2186221A (en) | Wing slot | |
GB519623A (en) | Improvements relating to arrangements for sucking-off the boundary layer on aeroplane wings | |
GB541078A (en) | Improvements in and relating to airscrews | |
GB530541A (en) | Improvements in and relating to aircraft | |
GB228637A (en) | Improvements in and relating to the supporting planes of aeroplanes | |
GB364337A (en) | Air craft wing | |
SU63901A1 (en) | Wing | |
FR841781A (en) | Aircraft lift wing, surface suction | |
GB660558A (en) | Improvements in or relating to aircraft wings | |
GB406485A (en) | Improvements in or relating to means for use in cooling aircraft motors | |
GB367880A (en) | Improvements relating to aircraft | |
GB518997A (en) | Improvements in parachutes | |
GB348293A (en) | An improved method of and means for reducing the air resistance of aircraft, motor cars, and other rapidly moving bodies | |
GB767257A (en) | Improvements in or relating to decoy aircraft |