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

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 PDF Author: Arthur L. Jones
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 78

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Book Description
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.

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

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 PDF Author: Arthur L. Jones
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 78

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Book Description
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

Sideslip Characteristics at Various Angles of Attack for Several Hypersonic Missile Configurations with Canard Controls at a Mach Number of 2.01 PDF Author: Gerald V. Foster
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 30

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Book Description


Aerodynamic Characteristics in Pitch and Sideslip of a 1/15-scale Model of the Scout Vehicle at a Mach Number of 2.01

Aerodynamic Characteristics in Pitch and Sideslip of a 1/15-scale Model of the Scout Vehicle at a Mach Number of 2.01 PDF Author: Ross B. Robinson
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 42

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Book Description


Jerry Coker's Complete Method for Improvisation

Jerry Coker's Complete Method for Improvisation PDF Author: Jerry Coker
Publisher: Alfred Music Publishing
ISBN: 9780769218564
Category : Music
Languages : en
Pages : 116

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Book Description
This uniquely organized method devotes a thorough chapter to each of the prevailing tune-types of jazz---standard, bebop, modal, blues, contemporary, ballad and free form---listing and discussing their characteristics and illustrating approaches to understanding and performing each type of tune. Includes CD.

Effect of Forebody Strakes on the Aerodynamic Characteristics in Pitch and Sideslip of a Hypersonic Airplane Configuration at Mach Numbers of 1.41, 2.01, and 6.86

Effect of Forebody Strakes on the Aerodynamic Characteristics in Pitch and Sideslip of a Hypersonic Airplane Configuration at Mach Numbers of 1.41, 2.01, and 6.86 PDF Author: Cornelius Driver
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 56

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The Dynamics of Vehicles on Roads and on Tracks

The Dynamics of Vehicles on Roads and on Tracks PDF Author: Robert Frohling
Publisher: CRC Press
ISBN: 1000443523
Category : Technology & Engineering
Languages : en
Pages : 804

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Book Description
These proceedings provide an authoritative source of information in the field of suspension design, vehicle-infrastructure interaction, mechatronics and vehicle control systems for road as well as rail vehicles. The research presented includes modelling and simulation.

Report

Report PDF Author:
Publisher:
ISBN:
Category : Automobiles
Languages : en
Pages : 544

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Book Description


Flight Testing of Fixed Wing Aircraft

Flight Testing of Fixed Wing Aircraft PDF Author: Ralph D. Kimberlin
Publisher: AIAA
ISBN: 9781600860560
Category : Airplanes
Languages : en
Pages : 464

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Book Description
Annotation The measurement of performance during an airplane's flight, testing is one of the more important tasks to be accomplished during its development as it impacts on both the airplane's safety and its marketability. This book discusses performance for both propeller-driven and jet aircraft.

The Yawing Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow

The Yawing Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow PDF Author: Arthur Leslie Jones
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 72

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

Automotive Control Systems

Automotive Control Systems PDF Author: Uwe Kiencke
Publisher: Springer Science & Business Media
ISBN: 3540231390
Category : Technology & Engineering
Languages : en
Pages : 522

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Book Description
Written by two of the most respected, experienced and well-known researchers and developers in the field (e.g., Kiencke worked at Bosch where he helped develop anti-breaking system and engine control; Nielsen has lead joint research projects with Scania AB, Mecel AB, Saab Automobile AB, Volvo AB, Fiat GM Powertrain AB, and DaimlerChrysler. Reflecting the trend to optimization through integrative approaches for engine, driveline and vehicle control, this valuable book enables control engineers to understand engine and vehicle models necessary for controller design and also introduces mechanical engineers to vehicle-specific signal processing and automatic control. Emphasis on measurement, comparisons between performance and modelling, and realistic examples derive from the authors’ unique industrial experience . The second edition offers new or expanded topics such as diesel-engine modelling, diagnosis and anti-jerking control, and vehicle modelling and parameter estimation. With only a few exceptions, the approaches