Sideslip

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Sideslip

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Author : R. J. Dunbar
language : en
Publisher:
Release Date : 2001-12-01

Sideslip written by R. J. Dunbar and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2001-12-01 with Fiction categories.

A Comparison Of Data Obtained By Two Flight Techniques For Determining The Sideslip Characteristics Of A Fighter Airplane

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Author : Harold I. Johnson
language : en
Publisher:
Release Date : 1945

A Comparison Of Data Obtained By Two Flight Techniques For Determining The Sideslip Characteristics Of A Fighter Airplane written by Harold I. Johnson 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: In order to determine the validity of sideslip data obtained in flight by the continuous-record method, sideslip data obtained from a fighter airplane in slowly increasing sideslips have been compared with sideslip data obtained from the same airplane in sideslips in which all the flight conditions were stabilized. The results of the comparison showed no essential difference in the sideslip characteristics obtained by the two flight techniques even though the continuous sideslips were purposely executed with a yawing velocity about double the usual rate of 1° per second in order to accentuate the effects of the small yawing and rolling velocities inherent in the method. Approximate theoretical calculations confirmed the experimental results but indicated that rates of yawing or rolling lower than 1° per second are desirable if the continuous-sideslip technique is employed in testing airplanes much larger than current fighters. The method of measuring sideslip characteristics under steady conditions is preferred to the method of measuring sideslip characteristics in slowly increasing sideslips when the airplane is directionally unstable, when is has a large pitching moment due to sideslip, or when a poor relationship exists among the rudder, aileron, and elevator control forces in sideslips.

The Effects Of Sideslip Aspect Ratio And Mach Number On The Lift And Pitching Moment Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow

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Author : Arthur L. Jones
language : en
Publisher:
Release Date : 1949

The Effects Of Sideslip Aspect Ratio And Mach Number On The Lift And Pitching Moment Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow written by Arthur L. Jones and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aerofoils categories.

The variations of lift and pitching moment with sideslip in supersonic flow have been calculated for a representative gorup of plan forms. The variations of lift and pitching moment with aspect ratio and Mach number at zero sideslip were also investigated. The analysis was based on linearized potential theory and was applied to triangular, trapezoidal, rectangular, and swept-back plan forms without dihedral.

Sideslip Characteristics At Various Angles Of Attack For Several Hypersonic Missile Configurations With Canard Controls At A Mach Number Of 2 01

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Author : Gerald V. Foster
language : en
Publisher:
Release Date : 1959

Sideslip Characteristics At Various Angles Of Attack For Several Hypersonic Missile Configurations With Canard Controls At A Mach Number Of 2 01 written by Gerald V. Foster and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamics, Supersonic categories.

The Yawing Moment Due To Sideslip Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow

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Author : Arthur Leslie Jones
language : en
Publisher:
Release Date : 1949

The Yawing Moment Due To Sideslip Of Triangular Trapezoidal And Related Plan Forms In Supersonic Flow written by Arthur Leslie Jones and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aerodynamics, Supersonic categories.

The variation of the yawing moment with sideslip and the variation of the stability derivative with aspect ratio and Mach number were investigated.

Aerodynamic Loading Characteristics In Sideslip Of A 45 Sweptback Wing With And Without A Fence At High Subsonic Speeds

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Author : Richard E. Kuhn
language : en
Publisher:
Release Date : 1955

Aerodynamic Loading Characteristics In Sideslip Of A 45 Sweptback Wing With And Without A Fence At High Subsonic Speeds written by Richard E. Kuhn and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Aerodynamic load categories.

Sideslip Angles And Vertical Tail Loads In Rolling Pull Out Maneuvers

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Author : Maurice D. White
language : en
Publisher:
Release Date : 1947

Sideslip Angles And Vertical Tail Loads In Rolling Pull Out Maneuvers written by Maurice D. White and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1947 with Airplanes categories.

Previous NACA reports have indicated that it is possible to develop angles of sideslip which may cause critical vertical-tail loads in abrupt rudder-fixed rolls from accelerated flight, but the reliability of methods for predicting these sideslip angles has not been demonstrated. In this report expressions for calculating the sideslip angles in these maneuvers are derived from theoretical considerations, and numerical solutions are obtained for a wide enough range of variables to permit construction of design charts. Comparison of the maximum sideslip angles obtained from the design charts and from flight tests with those obtained using a greatly simplified expression indicates sufficiently close agreement to warrant use of the simplified expression for first approximations in predicting sideslip angles and vertical-tail loads occurring in rolling pullout maneuvers for conventional ailerons. An approximate method for treating cases of nonlinear directional-stability characteristics is presented which gives reasonably good results. The vertical-tail loads measured on one airplane in rolling pull-out maneuvers corresponded closely with those calculated by the simplest methods when the actual sideslip angles attained were applied.

Sideslip

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Author : Ted White
language : en
Publisher: Hachette UK
Release Date : 2012-12-21

Sideslip written by Ted White and has been published by Hachette UK this book supported file pdf, txt, epub, kindle and other format this book has been release on 2012-12-21 with Fiction categories.

One minute I was in New York . . . walking down Sixth Avenue, a private eye on a two-bit job . . . Next minute I was in New York . . . a crazy town I almost recognised - but Goebbels was speaking in Union square, Hitler invited me to a cocktail party, and aliens from outer space were running the whole show. Fun City it wasn't . . . Plucked from his own "time", a pawn in a Galactic power play, Ron Archer fights his way through a deadly maze of intrigue and conspiracy to an incredible destiny at the end of the star lanes!

Flight Measurements Of The Rudder Control And Sideslip Characteristics Of Four Vertical Tail Arrangements On The P 40 Series Airplanes

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Author : Harold I. Johnson
language : en
Publisher:
Release Date : 1942

Flight Measurements Of The Rudder Control And Sideslip Characteristics Of Four Vertical Tail Arrangements On The P 40 Series Airplanes written by Harold I. Johnson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1942 with Aerodynamics categories.

Introduction: Directional control difficulties had been experienced in P-40 series airplanes in dive demonstrations and inadvertent entry into spins in service operations. At the request of the Army Air Forces, Materiel Command, quantitative measurements of rudder trim force change with speed and power, rudder force reversals in sideslips, and rudder positions in sideslips and straight flight of a P-40E airplane were made. Quantitative measurements of these items were also made on three other vertical tail arrangements supplied by the Curtiss-Wright Corporation. The results of these measurements are presented in this report.

An Analysis Of Incremental Horizontal Tail Loads Measured On A Swept Wing Bomber Airplane In Sideslip Maneuvers

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Author : William A. McGowan
language : en
Publisher:
Release Date : 1959

An Analysis Of Incremental Horizontal Tail Loads Measured On A Swept Wing Bomber Airplane In Sideslip Maneuvers written by William A. McGowan and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Mach number categories.