Author: Benjamin MilwitzkyPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 348
Book Description
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
Author: Benjamin MilwitzkyPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 348
Book Description
Report
Author: Report
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description
Annual Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Aero Digest
Author: High Speed Problems of Aircraft and Experimental Methods
Author: Allen F. DonovanPublisher: Princeton University Press
ISBN: 140087503X
Category : Science
Languages : en
Pages : 1021
Book Description
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.
The Interpretation of Nonlinear Pitching Moments in Relation to the Pitch-up Problem
Author: George S. CampbellPublisher:
ISBN:
Category : Mach number
Languages : en
Pages : 36
Book Description
NACA Conference on Aircraft Loads, Structures, and Flutter
Author: 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
Author: Clarence L. GillisPublisher:
ISBN:
Category : Mach number
Languages : en
Pages : 46
Book Description
Author: