Theoretical and Analog Studies of the Effects of Nonlinear Stability Derivatives on the Longitudinal Motions of an Aircraft in Response to Step Control Deflections and to the Influence of Proportional Automatic Control

Theoretical and Analog Studies of the Effects of Nonlinear Stability Derivatives on the Longitudinal Motions of an Aircraft in Response to Step Control Deflections and to the Influence of Proportional Automatic Control PDF Author: Benjamin Milwitzky
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 348

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Report

Report PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 962

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Report

Report PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32

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Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

The Interpretation of Nonlinear Pitching Moments in Relation to the Pitch-up Problem

The Interpretation of Nonlinear Pitching Moments in Relation to the Pitch-up Problem PDF Author: George S. Campbell
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 36

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Wing-on and Wing-off Longitudinal Characteristics of an Airplane Configuration Having a Thin Unswept Wing of Aspect Ratio 3, as Obtained from Rocket-propelled Models at Mach Numbers from 0.8 to 1.4

Wing-on and Wing-off Longitudinal Characteristics of an Airplane Configuration Having a Thin Unswept Wing of Aspect Ratio 3, as Obtained from Rocket-propelled Models at Mach Numbers from 0.8 to 1.4 PDF Author: Clarence L. Gillis
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Category : Mach number
Languages : en
Pages : 46

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Aero Digest

Aero Digest PDF Author:
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Category : Aeronautics
Languages : en
Pages : 1036

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High Speed Problems of Aircraft and Experimental Methods

High Speed Problems of Aircraft and Experimental Methods PDF Author: Allen F. Donovan
Publisher: Princeton University Press
ISBN: 140087503X
Category : Science
Languages : en
Pages : 1021

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Volume VIII of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: performance calculation at high speed; stability and control of high speed aircraft; aeroelasticity and flutter; model testing; transonic wind tunnels; supersonic tunnels; hypersonic experimental facilities; low density wind tunnels; shock tube; wind tunnel measurements; instrumented models in free flight; piloted aircraft testing; free flight range methods. Originally published in 1961. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

NASA Technical Note

NASA Technical Note PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 968

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NACA Conference on Aircraft Loads, Structures, and Flutter

NACA Conference on Aircraft Loads, Structures, and Flutter PDF Author:
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 702

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