The Time Vector Method for Lateral Stability Investigations

The Time Vector Method for Lateral Stability Investigations PDF Author: K. H. Doetsch
Publisher:
ISBN:
Category :
Languages : en
Pages : 42

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The Time Vector Method for Lateral Stability Investigations

The Time Vector Method for Lateral Stability Investigations PDF Author: K. H. Doetsch
Publisher:
ISBN:
Category :
Languages : en
Pages : 42

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The Time-vector Method for Lateral Stability Investigations

The Time-vector Method for Lateral Stability Investigations PDF Author: K. H. Doetsch
Publisher:
ISBN:
Category : Stability of airplanes, Lateral
Languages : en
Pages : 60

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Rocket-model Investigation of Lateral Stability Characteristics and Power Effects of a Jet-engine Airplane Configuration with Tail Boom at Mach Numbers from 1.15 to 1.37

Rocket-model Investigation of Lateral Stability Characteristics and Power Effects of a Jet-engine Airplane Configuration with Tail Boom at Mach Numbers from 1.15 to 1.37 PDF Author: T. Bradley Curry
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 34

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Determination of Lateral Stability Characteristics from Free-flight Model Tests, with Experimental Results on the Effects of Wing Vertical Position and Dihedral at Transonic Speeds

Determination of Lateral Stability Characteristics from Free-flight Model Tests, with Experimental Results on the Effects of Wing Vertical Position and Dihedral at Transonic Speeds PDF Author: Clarence L. Gillis
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 48

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A test and analysis method is presented for determining airplane lateral stability characteristics, including aerodynamic derivatives, from flight tests of scale models. The method of analysis utilizes the rotating time-vector concept and also a quasi-static approach. Data are presented at transonic speeds for three swept-wing rocket-propelled models differing only in vertical position and dihedral of the wing. The method proved to be adequate for delineating the major effects of the geometric variations on the aerodynamic lateral stability derivatives. The effects of Reynolds number on the linearity of the static stability data for an unswept wing configuration are illustrated.

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 938

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460

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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Parameter Estimation Techniques and Applications in Aircraft Flight Testing

Parameter Estimation Techniques and Applications in Aircraft Flight Testing PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 404

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NASA Technical Report

NASA Technical Report PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 50

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 300

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Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1048

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