Angle Of Yaw
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Angle Of Yaw
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Author : Ben Lerner
language : en
Publisher:
Release Date : 2006
Angle Of Yaw written by Ben Lerner and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2006 with Poetry categories.
"Angle of Yaw, Ben Lerner's ambitious second book of poetry, is an extended meditation on the commercialization of public space and speech. Combining philosophical insight with poetic experiment, political outrage with personal experience, Lerner's prose poems and lyrical sequences examine how technologies of viewing - aerial photography in particular - feed our spectacular culture an image of itself."--BOOK JACKET.
Angle Of Yaw
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Author : Ben Lerner
language : en
Publisher: Copper Canyon Press
Release Date : 2006-10-01
Angle Of Yaw written by Ben Lerner and has been published by Copper Canyon Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2006-10-01 with Poetry categories.
In his bold second book, Ben Lerner molds philosophical insight, political outrage, and personal experience into a devastating critique of mass society. Angle of Yaw investigates the fate of public space, public speech, and how the technologies of viewing—aerial photography in particular—feed our culture an image of itself. And it’s a spectacular view. The man observes the action on the field with the tiny television he brought to the stadium. He is topless, painted gold, bewigged. His exaggerated foam index finger indicates the giant screen upon which his own image is now displayed, a model of fanaticism. He watches the image of his watching the image on his portable TV on his portable TV. He suddenly stands with arms upraised and initiates the wave that will consume him. Haunted by our current “war on terror,” much of the book was written while Lerner was living in Madrid (at the time of the Atocha bombings and their political aftermath), as the author steeped himself in the history of Franco and fascism. Regardless of when or where it was written, Angle of Yaw will further establish Ben Lerner as one of our most intriguing and least predictable poets.
Effects Of Compressibility And Large Angles Of Yaw On Pressure Indicated By A Total Pressure Tube
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Author : Milton D. Humphreys
language : en
Publisher:
Release Date : 1945
Effects Of Compressibility And Large Angles Of Yaw On Pressure Indicated By A Total Pressure Tube written by Milton D. Humphreys and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1945 with Aerodynamics categories.
Summary: The effects of compressibility and angle of yaw on the pressure measured by a round-nose and a flat-nose total-pressure tube have been investigated. The tests were conducted in the Langley rectangular high-speed tunnel at Mach numbers from 0.3 to 0.9 for angles of yaw from 0° to 180°. The results indicated that no error was incurred in the measurement of total pressure by either tube for angles of yaw from 0° to 10° in the Mach number range investigated. At constant Mach numbers, the round-nose tube had a linear variation of total-pressure error with angle of yaw at angles ranging from 50° to 70°. This characteristic is desirable in yaw heads of the Y-type. The flat-nose tube had a nonlinear variation of total-pressure error with angle of yaw in this range.
Propellers In Yaw
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Author : Herbert S. Ribner
language : en
Publisher:
Release Date : 1943
Propellers In Yaw written by Herbert S. Ribner and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1943 with Aeronautics categories.
Summary: It was realized as early as 1909 that a propeller in yaw develops a side force like that of a fin. In 1917, R.G. Harris expressed this force in terms of the torque coefficient for the unyawed propeller. Of several attempts to express the side force directly in terms of the shape of the blades, however, none has been completely satisfactory. An analysis that incorporates induction effects not adequately covered in previous work and that gives good agreement with experiment over a wide range of operating conditions is presented herein. The present analysis shows that the fin analogy may be extended to the form of the side-force expression and that the effective fin area may be taken as the projected side area of the propeller. The effective aspect ratio is of the order of 8 and the appropriate dynamic pressure is roughly that at the propeller disk as augmented by the inflow. The variation of the inflow velocity, for a fixed-pitch propeller, accounts for most of the variation of side force with advance-diameter ration V/nD.
Effect Of Yaw And Angle Of Attack On Pressure Recovery And Mass Flow Characteristics Of A Rectangular Supersonic Scoop Inlet At A Mach Number Of 2 71
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Author : Raymond J. Comenzo
language : en
Publisher:
Release Date : 1954
Effect Of Yaw And Angle Of Attack On Pressure Recovery And Mass Flow Characteristics Of A Rectangular Supersonic Scoop Inlet At A Mach Number Of 2 71 written by Raymond J. Comenzo and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Jet engines categories.
Effects Of Yaw Angle And Reynolds Number On Rectangular Box Cavities At Subsonic And Transonic Speeds
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Author : Elizabeth B. Plentovich
language : en
Publisher:
Release Date : 1991
Effects Of Yaw Angle And Reynolds Number On Rectangular Box Cavities At Subsonic And Transonic Speeds written by Elizabeth B. Plentovich and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1991 with categories.
Formulas For Propellers In Yaw And Charts Of The Side Force Derivative
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Author : Herbert S. Ribner
language : en
Publisher:
Release Date : 1943
Formulas For Propellers In Yaw And Charts Of The Side Force Derivative written by Herbert S. Ribner and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1943 with Aeronautics categories.
Summary: General formulas are given for propellers for the rate of change of side-force coefficient with angle of yaw and for the rate of change of pitching-moment coefficient with angle of yaw. Charts of the side-force derivative are given for two propellers of different plan form. The charts cover solidities of two to six blades and single and dual rotation. The blade angles range from 15° or 20° to 60°. The equations, and the charts computed from the equations, are based on an unpublished analysis, which incorporates factors not adequately covered in previously published work and gives good agreement with experiment over a wide range of operating conditions. A study of the equations indicates that they are consistent with the following physical interpretation: In developing side force, the propeller acts like a fin of which the area is the projected side area of the propeller, the effective aspect ratio is of the order of 8, and the effective dynamic pressure is roughly that at the propeller disk as augmented by the inflow. The variation of the inflow velocity, for a fixed-pitch propeller, accounts for most of the variation of side force with advance-diameter ratio. The charts may be applied to obtain the rate of change of normal-force coefficient with angle of attack of the axis of rotation if proper account is taken of the upwash or downwash from the wing.
An Angle Of Attack And Angle Of Yaw Indicator Using A Direct Reading Simple Strain Gage Circuit On Sting Balances
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Author : Robert B. Ormsby
language : en
Publisher:
Release Date : 1954
An Angle Of Attack And Angle Of Yaw Indicator Using A Direct Reading Simple Strain Gage Circuit On Sting Balances written by Robert B. Ormsby and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Airplanes categories.
Wind Tunnel Investigation Of Effect Of Yaw On Lateral Stability Characteristics
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Author : Isidore G. Recant
language : en
Publisher:
Release Date : 1942
Wind Tunnel Investigation Of Effect Of Yaw On Lateral Stability Characteristics written by Isidore G. Recant and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1942 with Airplanes categories.
Combinations of an NACA 23012 tapered wing and a circular fuselage having a wedge-shaped rear were tested in the NACA 7- by 10-foot wind tunnel to determine the effect of wing-fuselage interference on the lateral-stability of wing-fuselage interference on the lateral-stability characteristics. The model configurations represented a high-wing, a mid-wing, and a low-wing monoplane. For each configuration, tests were made with a partial-span split flap neutral and deflected 60 degrees and with and without a vertical tail. Tests of the fuselage alone and of the fuselage with the vertical tail were also made.
The Lichtenberg Figures
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Author : Ben Lerner
language : en
Publisher: Copper Canyon Press
Release Date : 2013-10-10
The Lichtenberg Figures written by Ben Lerner and has been published by Copper Canyon Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2013-10-10 with Poetry categories.
Winner of the Hayden Carruth Award uses "broken sonnets" to explore complex juxtapositions of contemporary culture.