Approximate Corrections for the Effects of Compressibility on the Subsonic Stability Derivatives of Swept Wings PDF Download
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Author: Lewis R. Fisher
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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Book Description
A method which has previously been presented for the estimation of the low-speed stability derivatives of swept wings is modified to yield approximate corrections for the first-order three-dimensional effects of compressible flow in the subsonic region. Corrections are presented in chart for for several aspect ratios and angles of sweep. Lift-curve slopes and values of damping roll are compared with those obtained by use of a generally accepted method and are discussed in relation to unpublished data.
Author: Lewis R. Fisher
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
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Book Description
A method which has previously been presented for the estimation of the low-speed stability derivatives of swept wings is modified to yield approximate corrections for the first-order three-dimensional effects of compressible flow in the subsonic region. Corrections are presented in chart for for several aspect ratios and angles of sweep. Lift-curve slopes and values of damping roll are compared with those obtained by use of a generally accepted method and are discussed in relation to unpublished data.
Author: Lewis R. Fisher
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 35
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Book Description
A method which has previously been presented for the estimation of the low-speed stability derivatives of swept wings is modified to yield approximate corrections for the first-order three-dimensional effects of compressible flow in the subsonic region. Corrections are presented in chart for for several aspect ratios and angles of sweep. Lift-curve slopes and values of damping roll are compared with those obtained by use of a generally accepted method and are discussed in relation to unpublished data.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1200
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Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author: George C. Deutsch
Publisher:
ISBN:
Category : Carbides
Languages : en
Pages : 694
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Book Description
On a strength-to-weight ratio basis, ceramals appeared promising as gas-turbine-blade materials in the temperature range of 1600 to 2400 degrees F.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 940
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Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 694
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Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 396
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Book Description
Author: Anna M. Doro-on
Publisher: CRC Press
ISBN: 100065592X
Category : Political Science
Languages : en
Pages : 859
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Book Description
This book provides multifaceted components and full practical perspectives of systems engineering and risk management in security and defense operations with a focus on infrastructure and manpower control systems, missile design, space technology, satellites, intercontinental ballistic missiles, and space security. While there are many existing selections of systems engineering and risk management textbooks, there is no existing work that connects systems engineering and risk management concepts to solidify its usability in the entire security and defense actions. With this book Dr. Anna M. Doro-on rectifies the current imbalance. She provides a comprehensive overview of systems engineering and risk management before moving to deeper practical engineering principles integrated with newly developed concepts and examples based on industry and government methodologies. The chapters also cover related points including design principles for defeating and deactivating improvised explosive devices and land mines and security measures against kinds of threats. The book is designed for systems engineers in practice, political risk professionals, managers, policy makers, engineers in other engineering fields, scientists, decision makers in industry and government and to serve as a reference work in systems engineering and risk management courses with focus on security and defense operations.
Author: Howard F. Savage
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 662
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Book Description
An investigation has been conducted to determine the effects of vertical-tail location and size on the subsonic aerodynamic characteristics of a model having a triangular wing. The wing had an aspect ratio of 3, an NACA 0003.5-63 section in the streamwise direction, and plain, trailing-edge ailerons. The wing was attached to the fuselage in either a mid or high position and an unswept horizontal tail was located on the fuselage center line. Two vertical tails were tested which had areas of 26.7 or 20.3 percent of the wing area. Each vertical tail was equipped with a rudder and had a geometric aspect ratio of 1.5, a taper ratio of 0.16, and 54 degrees of sweepback of the leading edge. Each vertical tail was tested at two different tail lengths. The wind-tunnel tests were conducted at a Reynolds number of 2.5 milMon at Mach numbers from 0.25 to 0.95.
