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AMAZING DAY 2013
Back to the roots
Happy B.Day to Mr. WANY
15 - 16 - 17 Marzo
2013 – Locate Triulzi, MILANO.
That's the happening wait a sec daniel craig nicole kidman..WHAT leave the valley? VALLEY girls Forbidden planet BOOST Them and edumucation revoltion FOOL did you think your mind could contain all knowledge THE BOdy of christ..and at emmause...aristocrats and the booking agent sand sabir turns like urhura SET and shroom....until it become true I lie MAKE it so the truth and the booking agent holds up the phone "i'll" take them...ethopian dam UP reriver..who says they won't irrage to EYEPT says no muslim no satinst and the seedy MUSLim children weep...NO I just mean indoctrination ABBA FATHER and lionheart didn't go to jersuelem AS REPORTED and sadin didn't IT difficult enough as it is THE wide gate..and the valley girl get her Little baggy of 87% pure coke NOAH Less "work" MOre FAITH and drunky...THE called JIHad miliatia TIme to learn again ss cole..set where shroom all you learnt is BLARKARK? you know the cross that's what you know...and in this telling lionheart and saldin did MEET and then you can look it in..and LOSE IT stream reams CHEAP $10billion and hih collapse...SNOWAGEDDON on 1/2 gram of slurpy 2 boxes of lactose...and then the woopie cushion eyebrow raise THE MOP GUY...a christi in a reverse aution you know your bid..they'll kill "up" OBAMA to protect the middle classes..I WON the mop free mops and the old daughter of rome sat down FART...woopie cushions and the adidas puma conflict..at a THere up river in perpertuity % years, I mean 5 years in the flodding..the miliatia they called jihad they always call for a HOLY war and $2% that's the one you pass off..!&% IT's like ancient days snowgeddon this will put the full blood islanders outta business. THEY called jihad they want a holy war with china...gloria jeans the coffee of reeducation from the steepes to tiaman square
There's really notheing they can do THE great leader put his pland in PLACE I won
and cesear sat down HE thinks he's a friend..FART...a tactic that would work in any age STOP RAMBLING and the christians met IN SECRET YOU know better and everykid in rome wanted..the old daughter of rome was working on something TAHT's how you win a campaign like that and masda fell on their swords and the gurkas fell onm their swords...OH man the box set of convention weapons is sold out YOUTUBE to MP3 on line I have a whole album to listen to..I"M< looking at you they called jihad and back to ALEXANDER the great.
Reuters) - Ethiopia dismissed Egyptian talk of military action against a giant dam it is building on the Nile as "psychological warfare", and said on Tuesday it would defend itself and carry on with the work regardless.
Bellicose rhetoric between two of Africa's most populous and fastest-growing nations has raised fears of conflict over water, though both sides are also pursuing diplomatic compromise over what would be the biggest hydro electric plant on the continent
there UP river..DEFEND eypt with BLOOD..cause that law dates back to british imperialiam in colonisation
ADIDAS YEEZY BOOST 350 V2 RELEASE LINKS & INFO
supercopbot.com/2016/11/adidas-yeezy-boost-v2-release-lin...
The Best Sex Positions to Increase Chances of Pregnancy... read article @ www.justthefactsbaby.com/pregnancy/article/the-best-sex-p...
Schiemond | Lloydstraat
With the construction of the Shipping and Transport College, courses formerly spread throughout the city have been given a prominent place. The STC boosts the declining numbers of students in secondary and higher maritime education.
Arch. Neutelings Riedijk Architecten
2000-05.
delibrate boost of colors in PS, Merged two exposures together. Reflection on rocks and water is real.
Check it large on black to really enjoy this photograph
www.awaisyaqub.com/Landscapes/Kaghan-Valley-Pakistan/9366...
Io Aircraft - www.ioaircraft.com
Drew Blair
www.linkedin.com/in/drew-b-25485312/
io aircraft, phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air-Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, hypersonic plane, hypersonic aircraft, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, defense science, missile defense agency, aerospike,
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
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Moisés Naím, Senior Associate, International Economics, Carnegie Endowment for International Peace, USA at the World Economic Forum on Latin America in Panama City 2014. Copyright by World Economic Forum / Benedikt von Loebell
Un modèle rare de l'atelier Matsumoku au Japon, avec sa crosse copiée sur les Fender (par la suite le même modèle sdra produit avec la tête "maison"). Manche traversant, et switches à n'en plus finir, y compris un "volume boost" avec pile (donc, des micros actifs !).
Plus d'infos ici : www.greguti.com/guitares/ariaproiits600#.UWkWmlavTqB
The wrong boost gauge tubing kit can turn an afternoon project into a dramatic disappointment. It's simple really - tubing and fittings. What could possibly go wrong? Unfortunately, plenty.
Since 2002 we have been installing and selling boost gauges and various tubing kits. Over the years we have tested and developed many different solutions using a variety of fittings and tubing. Customer feedback has always been strong, letting us know what works and what doesn't. Throughout the years we've heard it all.
"my boost gauge buzzes"
"my tubing cracked, won't bend, melted, or isn't long enough"
"something's leaking"
"It just won't fit in my pod"
Updated for 2009, our tubing kits combine the best of the best at an affordable and competitive price. In the engine bay we're tapping into the factory intercooler plumbing with a miniature brass barb. Our brass barb uses miniature threads keeping your installation compact and discrete. At the gauge we're using our straight boost gauge fitting. This fitting is the most compact barb fitting we've ever found, allowing installation in the tightest of gauge pods. Tying it all together is 8 feet of the toughest and most flexible tubing we've ever used. Made from a high-tech polymer, our new tubing is flexible enough to bend around a quarter, but stiff enough to support itself without kinking or drooping. Our tubing can snake through gauge pods without kinking or crushing, while simultaneously holding tight on our barbed fittings without zip-ties or clamps. Spliced somewhere in-between, our proven inline restrictor provides a clean signal to the boost gauge. Zip ties and installation instructions are included for convenience.
Installing a boost gauge should be a simple task. Let's keep it that way.
Important Details
This kit is designed to be used on diesel engines with no available vacuum lines. This kit includes 8' of our flexible tubing, a barbed fitting to connect the tubing to the gauge, an inline restrictor, a brass barb to connect to the intercooler piping, zip-ties and installation instructions. Typical applications include mk4 TDI VW. Mk3 TDI VW's should use our standard tubing kit and tap the vacuum line which connects to the ECU.
Tubing Dimensions
.25" OD, .170" ID, 8' length
Boost Gauge Fitting Details
1/8" NPT female threads
.170" male barb
Inline Fitting Details
.1875" barbs
built-in vacuum restrictor
Brass Barb Details
.170" barb
#10-32 threads
Installation Instructions
Which tubing kit do I need?
We currently offer six boost gauge tubing kits. This kit is designed to install on engines with no available vacuum lines. The intake airstream is tapped by threading a brass barb into the intercooler plumbing. Choose your gauge fitting based on your mounting pod. Steering column mounted pods should use the 90 Degrees TDI Boost Gauge Tubing Kit.
We also offer a standard boost gauge tubing kit. The intake airstream is tapped using the included T-fitting. Follow the links below for information on our standard tubing kit. Standard kits are also available in straight or 90° configurations.
Boost Gauge Tubing Kit
90 Degrees Gauge Tubing Kit
We offer two MK5 tubing kits specifically designed to tap into the mk5 VW 2.0T FSI/TSI engine. The intake manifold is tapped using our MK5 Boost Gauge Tap. Follow the links below for information on our MK5 tubing kits in straight or 90° configurations.
MK5 Boost Gauge Tubing Kit
90 Degrees MK5 Boost Gauge Tubing Kit
The attention to detail on this Integra is nuts. If you haven't seen it in person you're missing out.
Canon EOS 7D 50mm 1.8
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91 Mazda Miata
PPG G35 Red Pearl
Greddy tdo4 15g turbo kit@11psi
Stripes FMIC kit
CX racing intercooler
HKS SSQV
test pipe
2 1/4 dual exhaust
Bipes/FMU
Walboro 190lph fuel pump
5spd converted
C's short shifter
Megan Racing coilovers
MS sway bars
Harddog Hardcore roll cage
01 hardtop
Project-G roof soiler
Autokonexion fender Flares
Touge Run duckbill spoiler
Moss Motors dual projectors
HID converted
Axis Sakura 15x8 0 offset front, -5 offset rear.
with spacers
coldtrackdays.blogspot.com/2009/06/eye-candy-honolulus-ho...