Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Pressure Measurements On The Apexes Of Two 60 Deg Sweptback Delta Wings Panel Semiapex Angle Of 30 Deg Having 0 Deg And 45 Deg Dihedral At A Mach Number Of 495
Download Pressure Measurements On The Apexes Of Two 60 Deg Sweptback Delta Wings Panel Semiapex Angle Of 30 Deg Having 0 Deg And 45 Deg Dihedral At A Mach Number Of 495 full books in PDF, epub, and Kindle. Read online Pressure Measurements On The Apexes Of Two 60 Deg Sweptback Delta Wings Panel Semiapex Angle Of 30 Deg Having 0 Deg And 45 Deg Dihedral At A Mach Number Of 495 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Challenge to Apollo by : Asif A. Siddiqi
Download or read book Challenge to Apollo written by Asif A. Siddiqi and published by www.Militarybookshop.CompanyUK. This book was released on 2011-03-01 with total page 1030 pages. Available in PDF, EPUB and Kindle. Book excerpt: Taking advantage of the Soviet archives, which were opened in the 1990s, Siddiqi has written a groundbreaking work that examines why the Soviet Union fell behind in the space race of the 1960s after changing the course of human history with the first artificial satellite launch, Sputnik, in 1957.
Book Synopsis Pressure Measurements on Two 60° Swept Delta Wings with Blunt Leading Edges and Dihedral Angles of 0° and 45° at a Mach Number of 4.95 by : P. Calvin Stainback
Download or read book Pressure Measurements on Two 60° Swept Delta Wings with Blunt Leading Edges and Dihedral Angles of 0° and 45° at a Mach Number of 4.95 written by P. Calvin Stainback and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Trichier written by Alessandra Ceretto and published by Lulu.com. This book was released on with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Flight Determination of the Tolerable Range of Effective Dihedral on a Conventional Fighter Airplane by : Charles J. Liddell
Download or read book A Flight Determination of the Tolerable Range of Effective Dihedral on a Conventional Fighter Airplane written by Charles J. Liddell and published by . This book was released on 1949 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: A conventional fighter airplane was equipped with a special device for varying the effective dihedral in flight. A survey of pilot's opinions was made to determine which values of effective dihedral were intolerable. The relation between the findings and the present Air Force-Navy stability and control specifications is discussed.
Book Synopsis Langley Full-scale-tunnel Investigation of the Fuselage Boundary Layer on a Typical Fighter Airplane with a Single Liquid-cooled Engine by : K. R. Czarnecki
Download or read book Langley Full-scale-tunnel Investigation of the Fuselage Boundary Layer on a Typical Fighter Airplane with a Single Liquid-cooled Engine written by K. R. Czarnecki and published by . This book was released on 1946 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made in the Langley full-scale tunnel to determine the thickness and shape of profile of the boundary layer on the fuselage of a typical monoplane fighter airplane with a single liquid-cooled engine. The results showed that, for the range of angles of attack and fuselage stations investigated, the maximum displacement thickness was nearly 1.2 inches and was at the most rearward station (81.6 percent of the fuselage length). The displacement thickness was found to be greatly affected by the pressure gradients over the windshield-canopy combination and in the wing-fuselage juncture. An average value for the shape parameter between 1.3 and 1.4 was obtained for the turbulent boundary layer.
Book Synopsis Earth Reflected Solar Radiation Incident Upon an Arbitrarily Oriented Spinning Flat Plate by : Fred G. Cunningham
Download or read book Earth Reflected Solar Radiation Incident Upon an Arbitrarily Oriented Spinning Flat Plate written by Fred G. Cunningham and published by . This book was released on 1963 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Notes on the Stalling of Vertical Tail Surfaces and on Fin Design by : F. L. Thompson
Download or read book Notes on the Stalling of Vertical Tail Surfaces and on Fin Design written by F. L. Thompson and published by . This book was released on 1940 with total page 566 pages. Available in PDF, EPUB and Kindle. Book excerpt: It may be concluded that the stalling of vertical tail surfaces is not in itself a dangerous condition. Provided sufficient directional stability exists at large angles of sideslip, the tail stall may occur with modern airplanes, as with those of the past, without the knowledge of or concern to the pilot.
Book Synopsis NASA Technical Translation by : United States. National Aeronautics and Space Administration
Download or read book NASA Technical Translation written by United States. National Aeronautics and Space Administration and published by . This book was released on 1970 with total page 230 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wartime Report ... A-. by : United States. National Advisory Committee for Aeronautics
Download or read book Wartime Report ... A-. written by United States. National Advisory Committee for Aeronautics and published by . This book was released on with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1977 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Technical Aerodynamics by : K. D. Wood
Download or read book Technical Aerodynamics written by K. D. Wood and published by Lulu.com. This book was released on 2019-11-15 with total page 530 pages. Available in PDF, EPUB and Kindle. Book excerpt: This is the third edition of a text much loved by engineers and aeronautical engineering students because it relates fundamental aerodynamic concepts to the practical facts of engineering design and teaches the two together. It is the companion to the 10th Edition (1954) of the same author's Airplane Design.In this improved facsimile edition, most of the front matter has been transcribed, the errata have been corrected, new headers and footers have been added and the pagination has been corrected so that odd pages are all on the right side. Some improvements have also been made to photos and line art.All other pages are page images of the original, printed Third Edition.
Book Synopsis Technical Aerodynamics by : Karl Dawson Wood
Download or read book Technical Aerodynamics written by Karl Dawson Wood and published by . This book was released on 1955-06 with total page 534 pages. Available in PDF, EPUB and Kindle. Book excerpt: This is the third edition of a text much loved by engineers and aeronautical engineering students because it relates fundamental aerodynamic concepts to the practical facts of engineering design and teaches the two together. It is the companion to the 10th Edition (1954) of the same author's Airplane Design. This improved reprint has most of the front matter transcribed, all errata corrected, new headers and footers instead of those in the page images, corrected pagination and section references and some improvements in the line art and photographs.
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781724666147 Total Pages :268 pages Book Rating :4.6/5 (661 download)
Book Synopsis Surface-Pressure and Flow-Visualization Data at Mach Number of 1. 60 for Three 65 Deg Delta Wings Varying in Leading-Edge Radius and Camber by : National Aeronautics and Space Administration (NASA)
Download or read book Surface-Pressure and Flow-Visualization Data at Mach Number of 1. 60 for Three 65 Deg Delta Wings Varying in Leading-Edge Radius and Camber written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-04 with total page 268 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation of the effect of leading-edge radius, camber, Reynolds number, and boundary-layer state on the incipient separation of a delta wing at supersonic speeds was conducted at the Langley Unitary Plan Wind Tunnel at Mach number of 1.60 over a free-stream Reynolds number range of 1 x 106 to 5 x 106 ft-1. The three delta wing models examined had a 65 deg swept leading edge and varied in cross-sectional shape: a sharp wedge, a 20:1 ellipse, and a 20:1 ellipse with a -9.750 circular camber imposed across the span. The wings were tested with and without transition grit applied. Surface-pressure coefficient data and flow-visualization data indicated that by rounding the wing leading edge or cambering the wing in the spanwise direction, the onset of leading-edge separation on a delta wing can be raised to a higher angle of attack than that observed on a sharp-edged delta wing. The data also showed that the onset of leading-edge separation can be raised to a higher angle of attack by forcing boundary-layer transition to occur closer to the wing leading edge by the application of grit or the increase in free-stream Reynolds number. McMillin, S. Naomi and Bryd, James E. and Parmar, Devendra S. and Bezos-OConnor, Gaudy M. and Forrest, Dana K. and Bowen, Susan Langley Research Center NASA-TM-4673, NAS 1.15:4673, L-17443 RTOP 505-59-53-05...
Book Synopsis The Soviet Space Race with Apollo by : Asif A. Siddiqi
Download or read book The Soviet Space Race with Apollo written by Asif A. Siddiqi and published by . This book was released on 2000 with total page 489 pages. Available in PDF, EPUB and Kindle. Book excerpt: Winner of the Emme Award for Astronautical Literature, 2001 "The essential reference work for Soviet/Russian space history . . . for anyone hoping to make sense of the too many 'truths' of Soviet Space history."--Journal of Military History "We finally have a definitive English-language history covering the first three decades of the Soviet Union's space program. Sixteen years in the making, Asif Siddiqi's amazingly detailed book provides a kaleidoscopic view of the technical and political evolution of Soviet missile and space projects. . . . a veritable gold-mind of factual information."--Air Power History "An extraordinary volume. . . . This is not simply an account of one side of the space race. It is nothing less than the first full-scale, detailed explanation of how and why the Soviet Union led the world into space. It belongs on the shelf of every historian with an interest in flight, technology and politics, the Cold War, or any one of a score of related topics."--The Public Historian "No space buff's library will be complete without this book. Readers will marvel at the complex interactions between design bureaus, and will enjoy getting to know the people behind the failed Soviet effort--a vital step toward putting Apollo's victory in context."--Smithsonian Air and Space "Absolutely mandatory on the bookshelf of anyone interested in space."--Encyclopedia Astronautica First published by NASA in 2000 as Challenge to Apollo, these two volumes are the first comprehensive history of the Soviet-manned space programs covering a period of thirty years, from the end of World War II, when the Soviets captured German rocket technology, to the collapse of their moon program in the mid-1970s. The spectacular Soviet successes of Sputnik--the first Earth satellite (1957) and Yuri Gagarin--the first man in space (1961) shocked U.S. leaders and prompted President John F. Kennedy to set the goal of landing a man on the moon before the end of the 1960s. The moon race culminated with the historic landing of Neil Armstrong and Buzz Aldrin on the moon in 1969 (coincidentally the first Soviet unmanned moon probe crashed on its surface while the American astronauts were at Tranquility Base). The epic story of the Soviet space program remained shrouded in secrecy until the unprecedented opening of top secret documents. Based almost entirely on these Russian-language sources and numerous interviews with veterans, Siddiqi's book breaks through the rumors, hearsay, and speculation that characterized books on the Soviet space program published during the Cold War years. Supplementing the text with dozens of previously classified photographs, he weaves together the technical, political, and personal history of the major Soviet space programs, providing the other side of the history of human space flight. Asif A. Siddiqi is a Ph.D. candidate in history at Carnegie Mellon University.
Book Synopsis Aerodynamic Characteristics of a Delta Wing with Leading Edge Swept Back 45 Degrees, Aspect Ratio 4, and NACA 65A006 Airfoil Section by : William C. Sleeman
Download or read book Aerodynamic Characteristics of a Delta Wing with Leading Edge Swept Back 45 Degrees, Aspect Ratio 4, and NACA 65A006 Airfoil Section written by William C. Sleeman and published by . This book was released on 1949 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper presents the results of the investigation of wing-alone and wing-fuselage combination employing a delta wing having 45 degree sweepback of the leading edge, aspect ratio 4, and an NACA 65A006 airfoil section. Lift, drag, pitching moment, and root bending moment were obtained for these configurations. In addition, effective downwash angles and dynamic-pressure characteristics in the region of a probable tail location also were obtained for these configurations, and are presented for a range of tail heights at one tail length. In order to expedite publishing of these data, only a brief analysis is included.
Book Synopsis Experimental Surface Pressure Data Obtained on 65 ̊delta Wing Across Reynolds Number and Mach Number Ranges by : Julio Chu
Download or read book Experimental Surface Pressure Data Obtained on 65 ̊delta Wing Across Reynolds Number and Mach Number Ranges written by Julio Chu and published by . This book was released on 1996 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723576270 Total Pages :518 pages Book Rating :4.5/5 (762 download)
Book Synopsis Experimental Surface Pressure Data Obtained on 65 Deg Delta Wing Across Reynolds Number and Mach Number Ranges. Volume 2; Small-Radius Leading Edge by : National Aeronautics and Space Administration (NASA)
Download or read book Experimental Surface Pressure Data Obtained on 65 Deg Delta Wing Across Reynolds Number and Mach Number Ranges. Volume 2; Small-Radius Leading Edge written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-24 with total page 518 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental wind tunnel test of a 65 deg. delta wing model with interchangeable leading edges was conducted in the Langley National Transonic Facility (NTF). The objective was to investigate the effects of Reynolds and Mach numbers on slender-wing leading-edge vortex flows with four values of wing leading-edge bluntness. Experimentally obtained pressure data are presented without analysis in tabulated and graphical formats across a Reynolds number range of 6 x 10(exp 6) to 84 x 10(exp 6) at a Mach number of 0.85 and across a Mach number range of 0.4 to 0.9 at Reynolds numbers of 6 x 10(exp 6) and 60 x 10(exp 6). Normal-force and pitching-moment coefficient plots for these Reynolds number and Mach number ranges are also presented. Chu, Julio and Luckring, James M. Langley Research Center NASA-TM-4645-Vol-2, L-17411B-Vol-2, NAS 1.15:4645-Vol-2 RTOP 505-59-54-01...
