NACA-University Conference on Aerodynamics, Construction, and Propulsion

NACA-University Conference on Aerodynamics, Construction, and Propulsion
Title NACA-University Conference on Aerodynamics, Construction, and Propulsion PDF eBook
Author United States. National Advisory Committee for Aeronautics
Publisher
Pages 462
Release 1954
Genre Aerodynamics
ISBN

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NACA-University Conference on Aerodynamics, Construction, and Propulsion

NACA-University Conference on Aerodynamics, Construction, and Propulsion
Title NACA-University Conference on Aerodynamics, Construction, and Propulsion PDF eBook
Author United States. National Advisory Committee for Aeronautics
Publisher
Pages 468
Release 1954
Genre Aerodynamics
ISBN

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Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics
Title Annual Report - National Advisory Committee for Aeronautics PDF eBook
Author United States. National Advisory Committee for Aeronautics
Publisher
Pages
Release 1957
Genre Aeronautics
ISBN

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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
Title 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 eBook
Author Dean R. Chapman
Publisher
Pages 206
Release 1958
Genre Aerofoils
ISBN

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NASA Technical Memorandum

NASA Technical Memorandum
Title NASA Technical Memorandum PDF eBook
Author
Publisher
Pages 92
Release 1982
Genre Aeronautics
ISBN

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Report

Report
Title Report PDF eBook
Author United States. National Advisory Committee for Aeronautics
Publisher
Pages 44
Release 1958
Genre Aeronautics
ISBN

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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
Title 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 eBook
Author Davis H. Crawford
Publisher
Pages 680
Release 1956
Genre Aeronautics
ISBN

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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.