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
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Total Pages : 348
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ISBN-10 : OSU:32435063878631
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Rating : 4/5 (31 Downloads)

Synopsis 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 by : Benjamin Milwitzky

Report

Report
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Publisher :
Total Pages : 962
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ISBN-10 : MINN:31951D00028207H
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Rating : 4/5 (7H Downloads)

Synopsis Report by :

Report

Report
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Publisher :
Total Pages : 32
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ISBN-10 : STANFORD:36105024791803
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Rating : 4/5 (03 Downloads)

Synopsis Report by : United States. National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics
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Total Pages :
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ISBN-10 : STANFORD:36105024166121
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Rating : 4/5 (21 Downloads)

Synopsis Annual Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

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

Aero Digest

Aero Digest
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Total Pages : 1036
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ISBN-10 : STANFORD:36105117568910
ISBN-13 :
Rating : 4/5 (10 Downloads)

Synopsis Aero Digest by :

High Speed Problems of Aircraft and Experimental Methods

High Speed Problems of Aircraft and Experimental Methods
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Publisher : Princeton University Press
Total Pages : 1021
Release :
ISBN-10 : 9781400875030
ISBN-13 : 140087503X
Rating : 4/5 (30 Downloads)

Synopsis High Speed Problems of Aircraft and Experimental Methods by : Allen F. Donovan

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.

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
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Publisher :
Total Pages : 46
Release :
ISBN-10 : UIUC:30112106741579
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Rating : 4/5 (79 Downloads)

Synopsis 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 by : Clarence L. Gillis

NASA Technical Note

NASA Technical Note
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Publisher :
Total Pages : 968
Release :
ISBN-10 : UOM:39015006101151
ISBN-13 :
Rating : 4/5 (51 Downloads)

Synopsis NASA Technical Note by :