Effect Of Horizontal Tail Size And Tail Length On Low Speed Static Longitudinal Stability And Damping In Pitch Of A Model Having 45 Sweptback Wing And Tail Surfaces PDF Download

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Effect of Horizontal-tail Size and Tail Length on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces

Effect of Horizontal-tail Size and Tail Length on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces
Author: Jacob H. Lichtenstein
Publisher:
Total Pages: 40
Release: 1951
Genre: Airplanes
ISBN:

Download Effect of Horizontal-tail Size and Tail Length on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces Book in PDF, ePub and Kindle

Wind-tunnel results of the effects of horizontal-tail size and length on the low-speed static longitudinal stability and the steady-state rotary damping in pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees and aspect ratios of 4 are presented.


Effect of Horizontal-tail Size and Tail Length on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Degrees Sweptback Wing and Tail Surfaces

Effect of Horizontal-tail Size and Tail Length on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Degrees Sweptback Wing and Tail Surfaces
Author: Jacob H. Lichtenstein
Publisher:
Total Pages: 32
Release: 1951
Genre: Airplanes
ISBN:

Download Effect of Horizontal-tail Size and Tail Length on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Degrees Sweptback Wing and Tail Surfaces Book in PDF, ePub and Kindle

Wind-tunnel results of the effects of horizontal-tail size and length on the low-speed static longitudinal stability and the steady-state rotary damping in pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees and aspect ratios of 4 are presented.


Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Degree Sweptback Wing and Tail Surfaces

Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Degree Sweptback Wing and Tail Surfaces
Author: Jacob H. Lichtenstein
Publisher:
Total Pages: 22
Release: 1952
Genre:
ISBN:

Download Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Degree Sweptback Wing and Tail Surfaces Book in PDF, ePub and Kindle


Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces

Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces
Author: Arthur Earl Bryson
Publisher:
Total Pages: 340
Release: 1952
Genre: Aeronautics
ISBN:

Download Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces Book in PDF, ePub and Kindle


Index of NACA Technical Publications

Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 274
Release: 1953
Genre: Aeronautics
ISBN:

Download Index of NACA Technical Publications Book in PDF, ePub and Kindle


NASA's Contributions to Aeronautics: Aerodynamics, structures, propulsion, controls

NASA's Contributions to Aeronautics: Aerodynamics, structures, propulsion, controls
Author:
Publisher:
Total Pages: 980
Release: 2010
Genre: Aeronautics
ISBN:

Download NASA's Contributions to Aeronautics: Aerodynamics, structures, propulsion, controls Book in PDF, ePub and Kindle

Two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, historians, museum curators, journalists, and independent scholars. Explores various aspects of how NACA-NASA research took aeronautics from the subsonic to the hypersonic era.-publisher description.