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Author : M. C. Leeka
Publisher : Honey Bear Books
ISBN 13 : 9781561449460
Total Pages : 36 pages
Book Rating : 4.4/5 (494 download)
Download or read book Nosing for Numbers written by M. C. Leeka and published by Honey Bear Books. This book was released on 1996-12 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Leo T. Chauvin
Publisher :
ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.3/5 (126 download)
Download or read book Pressure Distribution and Pressure Drag for a Hemispherical Nose at Mach Numbers 2.05, 2.54, and 2.04 written by Leo T. Chauvin and published by . This book was released on 1952 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: an experimental investigation of the pressure distributions on a hemispherical nose 3.98 inches in diameter, mounted on a cylindrical support, has been made at Mach numbers of 2.05, 2.54 and 3.04 and for Reynolds numbers of 4.44 x 106, 4.57 x 106, and 4.16 x 106, respectively. The Reynolds number was based on body diameter and free-stream conditions. Pressure-drag coefficients were calculated and good agreement was obtained between these tests and other investigations.
Author : Maurice A. Sylvester
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.3/5 (91 download)
Download or read book Wind Tunnel Tests of the Redstone "B" Nose Cone at Mach Numbers from 1.75 to 5.00 written by Maurice A. Sylvester and published by . This book was released on 1963 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : P. Calvin Stainback
Publisher :
ISBN 13 :
Total Pages : 82 pages
Book Rating : 4.:/5 (31 download)
Download or read book Effect of Unit Reynolds Number, Nose Bluntness, Angle of Attack, and Roughness on Transition on a 5° Half-angle Cone at Mach 8 written by P. Calvin Stainback and published by . This book was released on 1969 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : K. R. Czarnecki
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)
Download or read book Effects of Cone Angel, Mach Number, and Nose Blunting on Transition at Supersonic Speeds written by K. R. Czarnecki and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : J. Leith Potter
Publisher :
ISBN 13 :
Total Pages : 166 pages
Book Rating : 4.3/5 (91 download)
Download or read book Effects of Unit Reynolds Number, Nose Bluntness, and Roughness on Boundary Layer Transition written by J. Leith Potter and published by . This book was released on 1960 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt: Condtions encountered in the high Mach number flow regime are show to profoundly affect the longitudinal extent of the boundary layer from beginning to end of transition, the distribution of fluctuation energy in the laminar layer, and effectiveness of surface roughness in promoting transition. A critical layer of intense local energy fluctuations was found at all Mach numbers studied. The existence of such a critical layer is predicted by stability theory. Hot-wire surveys of the laminar, transitional, and turbulent boundary layers are presented to illustrate the critical layer in laminar flow and subsequent development into the transition process. The relation between boundary layer transition on flat plates and cones in supersonic flow is explored and a process for correcting data to account for leading edge bluntness is devised. On the basis of a comparison of data corrected for the effects of leading edge geometry, it is shown that the Reynolds umber of transition on a cone is three times that on a vanishingly thin flate plate. Close agreement between data from various wind tunnels is demonstrated. Study of the effect of finite leading edges yields significant illustrations of the influence of unit Reynolds number on boundary layer transition. A correlation of the effects of surface roughness on transition is achieved. This treatment includes two- and three-dimensional roughness in both subsonic and supersonic streams. At this time only zero pressure gradients have been studied. The entire range of movement of transition from its position with no roughness up to its reaching the roughness element is describable by the procedure give. Examples of application of the correlation results show excellent agreement with experimental data from a variety of sources. Implications concerning tripping hypersonic boundary layers are discussed.
Author : C. H. Wilts
Publisher :
ISBN 13 :
Total Pages : 362 pages
Book Rating : 4.3/5 (243 download)
Download or read book Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4 written by C. H. Wilts and published by . This book was released on 1958 with total page 362 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Robert E. Pendley
Publisher :
ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.3/5 (91 download)
Download or read book An Investigation of Several NACA 1-series Nose Inlets with and Without Protruding Central Bodies at High-subsonic Mach Numbers and at a Mach Number of 1.2 written by Robert E. Pendley and published by . This book was released on 1950 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of three NACA 1-series nose inlets, two of which were fitted with protruded central bodies, was conducted in the Langley 8-foot high-speed tunnel. An elliptical-nose body, which had a critical Mach number approximately equal to that of one of the nose inlets, was also tested. Tests were made near zero angle of attack for a Mach number range from 0.4 to 0.925 and for the supersonic Mach number of 1.2. The inlet-velocity-ratio range extended from zero to a maximum value of 1.34. Measurements included pressure distribution, external drag, and total-pressure loss of the internal flow near the inlet. Drag was not measured for the tests at the supersonic Mach number.
Author : Hans Florine
Publisher : Rowman & Littlefield
ISBN 13 : 149302499X
Total Pages : 240 pages
Book Rating : 4.4/5 (93 download)
Download or read book On the Nose written by Hans Florine and published by Rowman & Littlefield. This book was released on 2016-09-01 with total page 240 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hans Florine embodies the genius of "and"—collaborative and competitive, fast and safe, audacious and disciplined, visionary and quantitative. The themes that run through Florine's 101 ascents of Yosemite's most iconic route can benefit people who will never climb a rock, indeed anyone inspired by the idea of a passionate, lifelong quest of any type. —Jim Collins, author of Good to Great Hans Florine is a big-wall climbing legend in his own time. He holds the speed record on the Nose route of El Capitan, a 3,000-foot granite cliff in Yosemite Valley that’s considered the Everest of the rock-climbing world. Ascending the Nose takes most climbers anywhere from 12 to 96 hours. Florine, along with climbing partner Alex Honnold, does it in an astounding 2.5 hours. But Florine’s story is not one of super-human athletic prowess; it’s one of persistence and dogged determination. In 30 years of climbing, he's ascended the Nose a mind-blowing, death-defying 100 times, more than anyone else ever has, and most likely ever will. In On the Nose, Florine describes the most dangerous, pivotal, and inspirational of those climbs, providing a rare look inside the adrenaline-charged world of competitive climbing in Yosemite Valley. He tells of his very first attempt on the Nose, which ended in failure after 14 hours, his friendships (and rivalries) with climbing’s most colorful personalities, and his battle with Dean Potter to secure the definitive speed record on the Nose—an endeavor that’s been called the wildest competition known to man. Perhaps most interestingly, Florine attempts to answer the question why. Why would anyone undertake one of the greatest adventure epics on earth 100 times? His answers provide unique insights on how to live a satisfying life, how to achieve big goals, and how an otherwise ordinary guy can become a rock star.
Author : Benjamine J. Garland
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)
Download or read book Aerodynamic Heating and Boundary-layer Transition on a 1/10-power Nose Shape in Free Flight at Mach Numbers Up to 6.7 and Free-stream Reynolds Numbers Up to 16 X 10(6) written by Benjamine J. Garland and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Davis H. Crawford
Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (31 download)
Download or read book Investigation of the Flow Over a Spiked-nose Hemisphere-cylinder at a Mach Number of 6.8 written by Davis H. Crawford and published by . This book was released on 1959 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : William J. Monta
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (31 download)
Download or read book Effect of Nose Bluntness on Transition for a Cone and a Hollow Cylinder at Mach Numbers 1.41 and 2.01 written by William J. Monta and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John O. Reller (Jr.)
Publisher :
ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.3/5 (91 download)
Download or read book Heat Transfer to Blunt Nose Shapes with Laminar Boundary Layers at High Supersonic Speeds written by John O. Reller (Jr.) and published by . This book was released on 1957 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Robert D. Witcofski
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (31 download)
Download or read book Induced Pressures on Cylindrical Rods with Various Nose Drags and Nose Shapes at Mach Numbers of 17 and 21 written by Robert D. Witcofski and published by . This book was released on 1962 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Charles B. Rumsey
Publisher :
ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.:/5 (31 download)
Download or read book Heat-transfer Measurements on a Blunt Spherical-segment Nose to a Mach Number of 15.1 and Flight Performance of the Rocket-propelled Model to a Mach Number of 17.8 written by Charles B. Rumsey and published by . This book was released on 1959 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : David S. Shaw
Publisher :
ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.:/5 (31 download)
Download or read book Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Model Base on the Static Aerodynamic Characteristics of Blunt Bodies at Mach Numbers of 1.57, 1.80, and 2.16 and Angles of Attack Up to 180 ̊ written by David S. Shaw and published by . This book was released on 1963 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Anthony D. Cefalu
Publisher : AuthorHouse
ISBN 13 : 1456740792
Total Pages : 253 pages
Book Rating : 4.4/5 (567 download)
Download or read book Pull Your Nose Up written by Anthony D. Cefalu and published by AuthorHouse. This book was released on 2011-04-13 with total page 253 pages. Available in PDF, EPUB and Kindle. Book excerpt: A practical guide full of quick and easy to read ideas and advice for the seasoned business owner and novice sales professional alike, Pull You Nose Up is a must read for anyone looking to improve on their business operations and increase their sales results. In similar fashion to his first book, Sales Is a Contact Sport, Tony provides you with solid marketing and sales ideas to get things jump started in your business. Without all the fluff and double-speak common to so called experts, this book gives you the straight talk with such chapter titles as: -When Great Customer Service can Kill Your Business -All Customers are Created Equal; Some are More Equal than Others -Ideas are a Dime a Dozen, But their Execution is Priceless -To Make them Thirsty, Make the Well Run Dry -You are Not Responsible for Results; Just Right Behaviors -How Disturbing are You to People Pull Your Nose Up is the perfect book for the professional looking for a fresh new way of approaching sales and business operations and the one who is stuck for new ideas and new energy to get their business moving in the right direction. This book will do that for you.
