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