Server:GSE...
The main IP address: 208.91.197.27,Your server United States,Austin ISP:Network Solutions LLC TLD:com CountryCode:US
The description :eaa4 project for the kcgs hangar: lower weight -> lower costs via continuous fastening and laminar flow....
This report updates in 01-Aug-2018
Created Date: | 1996-10-02 |
Changed Date: | 2017-09-15 |
Geo IP provides you such as latitude, longitude and ISP (Internet Service Provider) etc. informations. Our GeoIP service found where is host schwenn.com. Currently, hosted in United States and its service provider is Network Solutions LLC .
Latitude: | 30.267150878906 |
Longitude: | -97.743057250977 |
Country: | United States (US) |
City: | Austin |
Region: | Texas |
ISP: | Network Solutions LLC |
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Server: | GSE |
Last-Modified: | Wed, 25 Jul 2018 14:20:28 GMT |
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Date: | Wed, 01 Aug 2018 09:29:22 GMT |
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ns: | ns89.worldnic.com. ns90.worldnic.com. |
ipv4: | IP:208.91.197.27 ASN:40034 OWNER:CONFLUENCE-NETWORK-INC - Confluence Networks Inc, VG Country:VG |
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navigation home an illustrative example project definition to-dos & questions to answer the team project updates laminar flow considerations stability & control for lighter planes challenges and difficulties benchmark dates files sitemap recent site activity 2857 days since project due date join our discussion join the discussion template tips learn more about working with templates. how to change this sidebar. home tip: how to replace these images with your own . overview this is a project to demonstrate and test a new method for constructing small aluminum airplanes - a method convenient to homebuilders and small manufacturers. the method should make significant laminar flow achievable in aluminum skin wings, lighten & strengthen the constructed plane, and much more. a 20% decrease in wing drag (other than induced which drops as speed increases) over a useful range of speeds and angles of attack makes for perhaps 5-10% overall drag, so a considerable fuel savings and/or a virtual increase in the engine's thrust for greater performance. laminar flow is the holy grail of aerodynamics - later on see why it could now be achieved by amateurs in aluminum. a principle achievement and practical goal of the method's consequences is a radical reduction in fuel costs. but a light, air- and water-tight, strong, vibration free plane presents many opportunities. the requirement is to build a forward-looking aviation project - with significant innovation. the innovation (the construction method and its implications) is meant to energize interest in general aviation, pilots, ex-pilots, would-be pilots, families, enthusiasts and journalists. ------------------------------ "continuous" fastenings (e.g. aviation fasteners vhb tape, epoxies, and welding films) are the key to the fastening method. they could enable (homebuilders included) to achieve extensive laminar flow in aluminum wing skin construction (and in some "internal" structures replace rivets and bolts with continuous weld). unlike similar materials put in use some time ago in airliner construction, these "adhesives" cure at temperatures (150f,250f) and clamping pressures easily and simply achieved by home builders and do not present the handling and toxicity issues of some welding methods and of liquid epoxies and other glues. (brazing material is now available which works at about 500f - low enough to leave the strength and shape of aluminum undisturbed. the brazed boundaries are stronger than the aluminum. another opening for the homebuilder.) eliminating virtually all surface riveting (and that of much internal structure) also permits the use of stronger (i. e. effectively lighter) alloys (e.g. 7075 & 2024) than rivet friendly 6061, and could save on the order of 500 hours of construction time. the project also takes advantage of an accident of general a viation's commercial history: the most common current engines are reliable but quite heavy and inefficient. reliable aviation engines are now available with -per horsepower- vastly lowered weight (by a factor of 2 to 3) and fuel consumption (by a factor of 3 to 4). their fuel is auto pump gas at less than 1/2 the cost of avgas. concretely, in one line: the project would build two identical aluminum wing sections with (potentially) laminar airfoil 64-415 (each with span of about 3-4 ribs), one span with conventional means, one with innovative "continuous fastener" means, then test and compare for strength and other flight relevant properties, including at least rough measurement of extent of laminar flow. messages rc modeler wanted who might like to build an rc model of our "target" airplane, much modified from "stock" (might be rv10-like, 172-like, sonerai-like or xenos-like.) there's one or two rv arf's available (4, 8 or 9 i think), infinite 172's, a sonerai plans built (which could also be modified to be xenos-like.)? it would be test flown, and would match more or less the x-plane model on the simulator. posted feb 3, 2016, 3:31 pm by peter schwenn we're on target... posted nov 30, 2015, 6:37 pm by peter schwenn the results of our survey... posted nov 30, 2015, 6:37 pm by peter schwenn showing posts 1 - 3 of 3 . view more ยป sign in | recent site activity | report abuse | print page | powered by google sites
http://www.schwenn.com/project-definition
http://www.schwenn.com/an-illustrative-example
http://www.schwenn.com/home/xenosvtail%20%281%29.jpg?attredirects=0
http://www.schwenn.com/the-team
http://www.schwenn.com/file-cabinet
http://www.schwenn.com/home/xenos_wing_010401_1.jpg?attredirects=0
http://www.schwenn.com/stability-control-for-lighter-planes
http://www.schwenn.com/system/app/pages/recentchanges
http://www.schwenn.com/calendar
http://www.schwenn.com/laminar-flow-considerations
http://www.schwenn.com/system/app/pages/sitemap/hierarchy
http://www.schwenn.com/project-updates/wereontarget
http://www.schwenn.com/to-dos
http://www.schwenn.com/project-updates
http://www.schwenn.com/project-updates/theresultsofoursurvey
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Domain Name: SCHWENN.COM
Registry Domain ID: 2691849_DOMAIN_COM-VRSN
Registrar WHOIS Server: whois.networksolutions.com
Registrar URL: http://networksolutions.com
Updated Date: 2017-09-15T18:25:52Z
Creation Date: 1996-10-02T04:00:00Z
Registry Expiry Date: 2020-10-01T04:00:00Z
Registrar: Network Solutions, LLC.
Registrar IANA ID: 2
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REGISTRAR Network Solutions, LLC.
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NAME schwenn.com
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NS89.WORLDNIC.COM 207.204.40.145
NS90.WORLDNIC.COM 207.204.21.145
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