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Low Angles
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Download or read book Low Angles written by Jim Stinson and published by Lulu.com. This book was released on 2007-01-01 with total page 186 pages. Available in PDF, EPUB and Kindle. Book excerpt: Against his better judgment, Stoney Winston arrives at a flea-bitten desert hamlet to help Diane LaMotta direct her first feature, a no-budget action potboiler titled (oh, please!) BIKERS FROM HELL. The director's hostile, the cameraman's drunk, the crew's rebelling, and the real bikers playing most of the parts act as bad as they smell. No problem. Diane and a luscious biker chick start fighting over Stoney's skinny bod. No problem. The production's slowly dying from systematic sabotage that escalates to stabbing, near-drowning, and violent death. That's a problem. Stoney's only weapons are his courage, his movie smarts, and his friend, Scuzzy. Courtly Nathaniel Hawthorne (Scuzzy) Fenster supports his rabbinical studies by playing biker roles in films; and since he stands six-six, weighs 300 pounds, and sprouts hair in all directions, the very sight of him would make Attila wet his pants. He works a lot.
Book Synopsis Laser Velocimeter Survey about a NACA 0012 Wing at Low Angles of Attack by : Danny R. Hoad
Download or read book Laser Velocimeter Survey about a NACA 0012 Wing at Low Angles of Attack written by Danny R. Hoad and published by . This book was released on 1978 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Flight written by and published by . This book was released on 1921 with total page 1336 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Design Charts for Predicting Downwash Angles and Wake Characteristics Behind Plain and Flapped Wings by : Abe Silverstein
Download or read book Design Charts for Predicting Downwash Angles and Wake Characteristics Behind Plain and Flapped Wings written by Abe Silverstein and published by . This book was released on 1939 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Several 6-percent-thick Airfoils at Angles of Attack from 0 to 20 Degrees at High Subsonic Speeds by : Bernard N. Daley
Download or read book Aerodynamic Characteristics of Several 6-percent-thick Airfoils at Angles of Attack from 0 to 20 Degrees at High Subsonic Speeds written by Bernard N. Daley and published by . This book was released on 1949 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two-dimensional tests of eight 6-percent-thick symmetrical airfoils of the supersonic and subsonic types were conducted in the Langley rectangular high-speed tunnel. The aerodynamic characteristics of each of the airfoils have been determined from the measured pressure data. These results showed that the lift-curve slope of each of the airfoils decreased rapidly to a positive value approaching zero at angles of attack near 9 degrees and roughly maintained this value up to the highest angle of attack tested.
Book Synopsis Apparent and Microscopic Contact Angles by : Kash L. Mittal
Download or read book Apparent and Microscopic Contact Angles written by Kash L. Mittal and published by CRC Press. This book was released on 2014-07-30 with total page 522 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book chronicles the proceedings of the International Symposium on Apparent and Microscopic Contact Angles, held in conjunction with the American Chemical Society meeting in Boston, August 24--27, 1998. The symposium provided an opportunity to discuss several controversial issues associated with interfacial phenomena that govern the behavior of
Book Synopsis Understanding Angles with Basketball by : Julia Wall
Download or read book Understanding Angles with Basketball written by Julia Wall and published by Capstone. This book was released on 2010-12 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: An exploration of angles that uses different aspects of basketball to explain vertex, kinds of angles, pivot, and other concepts.
Download or read book The Northern Microscopist written by and published by . This book was released on 1881 with total page 338 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Calculation of Magnus Forces on Axisymmetric Bodies at Small Angles of Attack with Incompressible Turbulent Boundary Layers by : Neal Tetervin
Download or read book Calculation of Magnus Forces on Axisymmetric Bodies at Small Angles of Attack with Incompressible Turbulent Boundary Layers written by Neal Tetervin and published by . This book was released on 1972 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Magnus force is found by adding the boundary layer displacement surface to the body and then calculating the force on the resulting non- axisymmetric body. The displacement surface is calculated by the simultaneous integration of a differential equation for a streamline, two partial-differential boundary layer integral-momentum equations with the boundary layer thickness and the tangent of the angle between the local direction of the surface friction and potential flow streamline as dependent variables, and a partial differential equation for the displacement surface thickness. The method is applied to a half-ellipsoid of fineness ratio 5 at 4 degrees angle of attack. Slender-body theory is used to calculate the force.
Book Synopsis Aviation and Aeronautical Engineering by :
Download or read book Aviation and Aeronautical Engineering written by and published by . This book was released on 1920 with total page 294 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aviation Week & Space Technology by :
Download or read book Aviation Week & Space Technology written by and published by . This book was released on 1920 with total page 512 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Technical Report of the Advisory Committee for Aeronautics for the Year ... by :
Download or read book Technical Report of the Advisory Committee for Aeronautics for the Year ... written by and published by . This book was released on 1919 with total page 736 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wartime Report written by and published by . This book was released on 194? with total page 746 pages. Available in PDF, EPUB and Kindle. Book excerpt: Reproductions of reports, some declassified, of research done at Langley Memorial Aeronautical Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.
Book Synopsis Technical Report by : Aeronautical Research Council (Great Britain)
Download or read book Technical Report written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1919 with total page 722 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes its Reports, which are also issued separately.
Book Synopsis Model Aviation ABC by : Martin Simons
Download or read book Model Aviation ABC written by Martin Simons and published by Verlag für Technik und Handwerk. This book was released on with total page 211 pages. Available in PDF, EPUB and Kindle. Book excerpt: Martin Simons, a passionate model pilot and multiple book author about the basics of model flying and aerodynamics, describes in an entertaining way why and how models fly in his book "Modellflug-ABC". With his clear and easy to understand language, he succeeds in summarizing even complex topics. For both beginners and advanced pilots, "Model Aviation ABC" is a valuable aid to understanding when and why models fly well, and how to use this knowledge to expand and refine your own flying skills. From the Content: In "Model Aviation ABC" the basics of aerodynamics (without mathematical deepening) are explained in connection with model flying, e.g. to clarify the effect of control reactions. What is the effect of a symmetrical or a semi-symmetrical airfoil? What triggers a stall and how do you recover the model? What makes a model stable and how do I achieve high stability? What is the importance of the propeller? Many questions that arise in the everyday life of model pilots are answered in the "Model Aviation ABC" in an explanatory way. The goal is to know and understand aerodynamic processes to set up and fly models well. Over 100 drawings illustrate the processes described in the text and round off the basics taught in the "Model Aviation ABC".
Book Synopsis Aeronautics by : Matthias Nace Forney
Download or read book Aeronautics written by Matthias Nace Forney and published by . This book was released on 1893 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Aerodynamic Characteristics of a Low-Drag Aircraft Configuration Having an Arrow Wing of Aspect Ratio 1.86 and a Body of Fineness Ratio 20 by :
Download or read book Supersonic Aerodynamic Characteristics of a Low-Drag Aircraft Configuration Having an Arrow Wing of Aspect Ratio 1.86 and a Body of Fineness Ratio 20 written by and published by . This book was released on 1960 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: A free-flight rocket-propelled-model investigation was conducted at Mach numbers of 1.2 to 1.9 to determine the longitudinal and lateral aero-dynamic characteristics of a low-drag aircraft configuration. The model consisted of an aspect-ratio -1.86 arrow wing with 67.5 deg. leading-edge sweep and NACA 65A004 airfoil section and a triangular vertical tail with 60 deg. sweep and NACA 65A003 section in combination with a body of fineness ratio 20. Aerodynamic data in pitch, yaw, and roll were obtained from transient motions induced by small pulse rockets firing at intervals in the pitch and yaw directions. From the results of this brief aerodynamic investigation, it is observed that very slender body shapes can provide increased volumetric capacity with little or no increase in zero-lift drag and that body fineness ratios of the order of 20 should be considered in the design of long-range supersonic aircraft. The zero-lift drag and the drag-due-to-lift parameter of the test configuration varied linearly with Mach number. The maximum lift-drag ratio was 7.0 at a Mach number of 1.25 and decreased slightly to a value of 6.6 at a Mach number of 1.81. The optimum lift coefficient, normal-force-curve slope, lateral-force-curve slope, static stability in pitch and yaw, time to damp to one-half amplitude in pitch and yaw, the sum of the rotary damping derivatives in pitch and also in yaw, and the static rolling derivatives all decreased with an increase in Mach number. Values of certain rolling derivatives were obtained by application of the least-squares method to the differential equation of rolling motion. A comparison of the experimental and calculated total rolling-moment-coefficient variation during transient oscillations of the model indicated good agreement when the damping-in-roll contribution was included with the static rolling-moment terms.
