links · people · groups · tags | My: links · tags · groups · watchlists · notes login · sign up now! | help · blog
Simpy simpy
 
Michael Shook, member since May 27, 2004
.
Search Everyone: "physics",

Top "physics" experts: klaus, tuuli, stargaming, rmerkus, tomhgxx, gdw,

Groups about "physics": Physical Education and Coaching, Science, SEEKER FINDER, Hand Drumming and the Djembe , Health and Body, free science online,

1 - 10 of 14 next »   Watch mshook
 
via http://nikolledoolin.com/pblog/?p=184
via http://librivox.org/the-turn-of-the-screw-by-henry-james/

Categories
Amazon Kindle
Apple
Art
Audio Books
Blogs
Books
Business
Comedy
Current Affairs
e-books
Economics
Education
English Language
Environment
Film
Foreign Language
Google
Harvard
History
iPhone
Law
Life
Literature
Math
Media
MIT
Most Popular
Music
Online Courses
Philosophy
Physics
Podcast Articles and Resources
Politics
Psychology
Random
Religion
Sci Fi
Science
Stanford
Technology
Television
Theater
Twitter
UC Berkeley
Uncategorized
Video – Arts & Culture
Video – Politics/Society
Video – Science
Web/Tech
Weblogs
Wikipedia
Yale
YouTube
by mshook 2009-10-12 10:33 eclectic · culture · science · interesting · via · librivox · blog · media · economics · philosophy · physics · religion · harvard · mit · worthwhile
http://www.openculture.com/ - cached - mail it - history

When I push [my toaster] lever down, if there's a crumb stuck in the coils, it isn't long before my fragile pre-coffee state is shattered by the piercing siren of my smoke detector. It doesn't know about the toast, but really it should. If it were sociable, as soon as it detected particulate matter in the air, it would query the toaster to see if it had been activated. That would tell it that in all likelihood, it wasn't detecting an unattended, middle-of-the-night fire but instead a benign morning meal. The price of low-power radio networking and the just-minted funding for smart home energy networks makes this sociable smoke-detector scenario entirely within our reach. I want one.

by mshook 2009-08-18 09:49 zigbee · mesh · network · social · ubiquitous · physical · computing · nyu · emon · electricity · projects · interesting
http://www.computerworld.com/s/article/print/335788/Rob_Faludi?taxonomyName=Networking+and+Internet&taxonomyId=16 - cached - mail it - history
http://www.make-digital.com/make/vol17/?pg=139 http://www.make-digital.com/make/vol17/?pg=142
by mshook 2009-03-07 12:38 music · project · electronics · led · make · synth · physical · sound · video · schematic · circuit · wav · via · borders · march · 2009
http://makezine.com/17/diymusic_elasticbass/ - cached - mail it - history
"# The Telegraph---History of the Electromagnetic Telegraph; Telegraph and Telecommunications Lore # Egypt, Greece and Rome---Latin and Greek Lessons, Geometry and Egyptian Notes # Railways---Railway History and Engineering, Especially Signalling and Operation # American History---Historical Notes of All Kinds; William Henry Harrison; Heraldry # Physics---Physics and Chemistry; Electromagnetism; Quantum Mechanics; Group Theory; The Hodograph # Mathematical Physics---Physics Through Mathematics, from Analytical Mechanics to Relativity "
by mshook 2008-08-04 21:32 interesting · eclectic · engineering · england · rail · train · railroad · telephone · telegraph · history · physics · wave · sound · stats · oil
http://mysite.du.edu/~jcalvert/index.htm - cached - mail it - history
"The Actuator Disc Theory: This first practical theory of propellers was developed by Rankine in 1865, extended by R. E. Froude in 1886. The theory stated that force (thrust) equals the mass times acceleration of the fluid. It gives no information on geometry but gives the ideal efficiency of a propeller. The Blade Element Theory: States that blade element equals radial cross-section of a blade. The total force (thrust and torque) on a propeller blade is determined by analyzing the forces on each blade element (W. Froude, 1878 and Taylor 1893). Unfortunately this leads to erroneous results that ideal efficiency of a propeller is unity. "
by mshook 2007-10-23 15:00 propeller · navy · cfd · history · analysis · physics · theory
http://www.dt.navy.mil/pao/excerpts pages/1998/proplect7.html - cached - mail it - history
via http://www.lecun.org/hobby/links.html
by mshook 2007-09-10 03:16 aero · airplane · flight · how · ebook · book · physics · why · cfd
http://www.av8n.com/how/ - cached - mail it - history
"Using the quite simple momentum theory, we can already deduct important information about the performance of propellers. We can study the influence of the propeller diameter on efficiency as well as how it depends on flight speed or the density of the air (corresponding to a certain altitude). We learn, that an efficient propeller should have a small power loading per disk area, i.e. a large diameter is required. The momentum theory does neither take the planform of the blade into account nor the characteristics of the airfoil sections. For the design or the analysis of a propeller more sophisticated models are necessary, but the momentum theory always gives a good estimate for the maximum efficiency which we can expect. It is possible to extend the momentum theory to include rotational losses, which results in an additional efficiency loss of 2 to 5 percent for typical propellers. These losses depend on the velocity of rotation and favor low torque, high rpm conditions. "
by mshook 2007-08-23 20:02 propeller · theory · helicopter · physics · momentum · how · math
http://www.mh-aerotools.de/airfoils/propuls4.htm - cached - mail it - history
"physics behind vertical flight is described by the author as 'momentum theory', which was developed for marine propellors in the late nineteenth century. As the name implies, this is just an application of the principle of conservation of momentum. The rotor disk of the helicopter feels a thrust created by the action of the air on the helicopter blades. It must therefore exert an equal and opposite force on the air. This forces the velocity of the air in the rotor wake to be opposite in direction to the direction of the thrust. Momentum conservation, energy conservation, and mass conservation then give a relation between the induced power loss and the rotor thrust. The author also gives details on the 'vortex theory', which is based more on fluid dynamical laws of the flow field of the rotor wake. Emphasizing the local aspects, it reduces to momentum theory in appropriate limits. The author also shows how momentum theory applies to the forward flight of the helicopter. The author also treats helicopter performance analysis, which boils down to determining the power required and available for a range of flight conditions. The rotor forces and power must be calculated, and the author details two methods to do this: the 'force balance method' and the 'energy balance method'. The use of the computer has made this analysis considerably easier for the design engineer of course. The author gives a very interesting overview of helicopter speed limitations and how the helicopter could be landed safely after an engine failure, all of this being analyzed from a physics perspective. The mathematics of rotating systems is included in the book, along with the differential equations of motion for the rotor blade. The motion of the blade is expanded into a normal mode representation and analyzed using Sturm-Liouville theory. The author though outlines other approaches to the blade dynamics, such as the Lagrangian formulation and the Galerkin method. And also, in spite of the ability of computers to solve for the aeroelastic equations of motion, the author considers their analytical solution for the cases where such solutions can be obtained. One very interesting part of this discussion was that of 'ground resonance', which is a dynamic instability involving the the coupling of the blade lag motion with the in-plane motion of the rotor hub. There is then a resonance between the frequency of the rotor lag motion and the natural frequency of the structure supporting the rotor. "
by mshook 2007-08-23 19:42 book · lookinside · helicopyter · physics · theory · 0486682307 · isbn0486682307 · marine · propeller · review
http://www.amazon.com/Helicopter-Theory-Wayne-Johnson/dp/0486682307/ - cached - mail it - history
"Written for everyone from motorcycling greenhorns to technical experts, this illustrated tour of motorcycle physics and mechanics offers a complete presentation of concepts which have never before been so thoroughly and comprehensibly presented in print. After examining the physical phenomena that govern the handling of a motorcycle, the text goes on to explain the various types of components that come together and make the bike go. Applicable to all makes and models, a generous selection of illustrations and photographs help readers visualize the topics at hand, allowing them to hit the saddle with a more complete awareness that enhances the riding experience. --This text refers to an out of print or unavailable edition of this title."
by mshook 2007-08-16 23:44 motorcycle · design · technology · why · frame · physics · via · borders · book · searchinside
http://www.amazon.com/Motorcycle-Design-Technology-Gaetano-Cocco/dp/8879113445/ - cached - mail it - history
"Brake Mean Effective Pressure (BMEP) is another very effective yardstick for comparing the performance of one engine to another, and for evaluating the reasonableness of performance claims or requirements. The definition of BMEP is: the average (mean) pressure which, if imposed on the pistons uniformly from the top to the bottom of each power stroke, would produce the measured (brake) power output. Note that BMEP is purely theoretical and has nothing to do with actual cylinder pressures. It is simply an effective comparison tool. If you work through the arithmetic, you find that BMEP is simply a multiple of the torque per cubic inch of displacement. A torque output of 1.0 lb-ft per cubic inch of displacement equals a BMEP of 150.8 psi. in a four-stroke engine and 75.4 psi. in a two-stroke engine. (The discussion on the remainder of this page is with respect to four-stroke engines, but it applies equally to two strike engines if you simply substitute 75.4 everywhere you see 150.8) If you know the torque and displacement of an engine, a very practical way to calculate BMEP is: BMEP = 150.8 x TORQUE (lb-ft) / DISPLACEMENT (ci) (equation 8) This tool is extremely handy to evaluate the performance which is claimed for any particular engine. For example, the 200 HP IO-360 (360 CID) and 300 HP IO-540 (540 CID) Lycomings make their rated power at 2700 RPM. At that RPM, the rated power requires 389 lb-ft and 584 lb-ft of torque respectively. (If you don't understand that calculation, CLICK HERE). From those torque values, it is easy to see (from equation 8 above) that both engines operate at a BMEP of about 163 PSI. (1.08 lb-ft of torque per cubic inch) at peak power. The BMEP at peak torque is slightly greater. For a long-life, naturally-aspirated, gasoline-fueled, two-valve-per-cylinder, pushrod engine, a BMEP over 200 PSI is difficult to achieve and requires a serious development program and very specialized components. For comparison purposes, let's look at what is commonly believed to be the very pinnacle of engine performance: Formula-1 (Grand Prix). An F1 engine is purpose-built and essentially unrestricted. For 2006, the rules required a 90° V8 engine of 2.4 liters displacement (146.4 CID) with a maximum bore of 98mm (3.858) and a required bore spacing of 106.5 mm (4.193). The resulting stroke to achieve 2.4 liters is 39.75 mm (1.565) and is implemented with a 180° crankshaft. The typical rod length is approximately 3.94, for a Rod/Stroke ratio of about 2.51. These engines are typically a 4-valve-per cylinder layout with two overhead cams per bank, and use pneumatic valvesprings. In addition to the few restrictions stated above, there are the following additional restrictions: (a) no beryllium compounds, (b) no MMC pistons, (c) no variable-length intake pipes, (d) one injector per cylinder, and (e) the requirement that one engine last for two race weekends. At the end of the 2006 season, these F1 engines made in the vicinity of 750 HP at an astonishing 19,000 RPM. Assuming peak power is around 18,500, the torque at peak power would be 213 lb-ft and peak-power BMEP would be 219 psi. Peak torque BMEP would likely be at least 10 psi greater. There can be no argument that 219 psi at 18,500 RPM is truly amazing. However, let's look at some astounding domestic technology. The 2006 Nextel Cup engine is a severely-restricted powerplant, being derived from production components. It is based on a production cast-iron 90° V8 block and 90° crankshaft, with a maximum displacement of 358 CID (5.87 liters). A typical configuration has a 4.185" bore with a 3.25" stroke and a 6.20" conrod (R/S = 1.91). Cylinder heads are similarly production-based, limited to two valves per cylinder. The valves are operated by a single, engineblock-mounted, flat-tappet camshaft (that's right, still no rollers as of 2007) and a pushrod / rocker-arm / coil-spring valvetrain. It is further hobbled by the requirement for a single four-barrel carburetor. Electronically-controlled ignition is not allowed, and there are minimum weight requirements for the conrods and pistons. How does it perform? At the end of the 2006 season, the engines were producing in the neighborhood of 840 HP at 9000 RPM (and could produce more at 10,000 RPM, but engine RPM has been restricted by means of a rule limiting the final drive ratio at each venue). 840 HP at 9000 RPM requires 490 lb-ft of torque, for a peak-power BMEP exceeding 206 PSI. Estimating peak torque to be 550 lb-ft (probably in the neighborhood of 7800 RPM) yields a peak BMEP of nearly 232 PSI. THAT is truly astonishing. To appreciate the value of this tool, suppose someone offers to sell you a 2.8 liter (171 cubic inch) Ford V6 which allegedly makes 230 HP at 5000 RPM, and is equipped with the standard iron heads and an aftermarket intake manifold and camshaft. You could evaluate the reasonableness of this claim by calculating that 230 HP at 5000 RPM requires 242 lb-ft of torque (230 x 5252 ÷ 5000), and that 242 lb-ft. of torque from 171 cubic inches requires a BMEP of 213 PSI (150.8 x 242 ÷ 171). You would then dismiss the claim as preposterous because you know that if a guy could do the magic required to make that kind of performance with the stock heads and intake design, he would be renowned as one of the pre-eminent engine gurus in the world. (You would later discover that the engine rating of "230" is actually "Blantonpower", not Horsepower.) As a matter of fact, in order to get a BMEP value of 214 from our aircraft V8, we had to use extremely well developed, high-flowing, high velocity heads, a specially-developed tuned intake and fuel injection system, very well developed cam profiles and valve train components, and a host of very specialized components which we designed and manufactured."
by mshook 2007-08-07 22:41 engine · aero · auto · physics · ic · power · pressure · heat
http://www.epi-eng.com/ET-BMEP.htm - cached - mail it - history
1 - 10 of 14 next »  
Related Tags
 
- exclude ~ optional + require
Add Dates