NACA-University Conference on Aerodynamics, Construction, and Propulsion

NACA-University Conference on Aerodynamics, Construction, and Propulsion PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 462

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NACA-University Conference on Aerodynamics, Construction, and Propulsion

NACA-University Conference on Aerodynamics, Construction, and Propulsion PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 462

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Book Description


NACA-University Conference on Aerodynamics, Construction, and Propulsion

NACA-University Conference on Aerodynamics, Construction, and Propulsion PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 462

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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.

Experimental Determination of Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Upswept Wing Oscillating in Yaw

Experimental Determination of Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Upswept Wing Oscillating in Yaw PDF Author: Dean R. Chapman
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 206

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 92

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Report

Report PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 44

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Investigation of the Laminar Aerodynamic Heat-transfer Characteristics of a Hemisphere-cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8

Investigation of the Laminar Aerodynamic Heat-transfer Characteristics of a Hemisphere-cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8 PDF Author: Davis H. Crawford
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 680

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At the stagnation point, the theory of Sibulkin, using the diameter and conditions behind the normal shock, was in good agreement with the experiment when the velocity graident at the stagnation opint appropriate to the free-stream Mach number was used.

Report

Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1180

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Aerodynamic Components of Aircraft at High Speeds

Aerodynamic Components of Aircraft at High Speeds PDF Author: Allen F. Donovan
Publisher: Princeton University Press
ISBN: 1400879906
Category : Science
Languages : en
Pages : 863

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Book Description
Volume VII of the High Speed Aerodynamics and Jet Propulsion series. It deals with applications to specific components of the complete aircraft. Sections of the volume include: aerodynamics of wings at high speed, aerodynamics of bodies at high speed, interaction problems, propellers at high speed, diffusers and nozzles, and nonsteady wing characteristics. Originally published in 1957. 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.

Analytic Methods in Aircraft Aerodynamics

Analytic Methods in Aircraft Aerodynamics PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 758

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