Scientific and Technical Aerospace Reports PDF Download
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Author:
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Category : Aeronautics
Languages : en
Pages : 440
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 440
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ISBN:
Category : Government publications
Languages : en
Pages : 856
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Category : Government publications
Languages : en
Pages : 854
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Author: Mark C. Davis
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Category : Aerodynamics, Hypersonic
Languages : en
Pages : 28
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NASA Dryden Flight Research Center has developed a flush airdata sensing (FADS) system on a sharp-nosed, wedge-shaped vehicle. This paper details the design and calibration of a real-time angle-of-attack estimation scheme developed to meet the onboard airdata measurement requirements for a research vehicle equipped with a supersonic-combustion ramjet engine. The FADS system has been designed to perform in flights at speeds between Mach 3 and Mach 8 and at angles of attack between -6° and 12°. The description of the FADS architecture includes port layout, pneumatic design, and hardware integration. Predictive models of static and dynamic performance are compared with wind-tunnel results across Mach and angle-of-attack range. Results indicate that static angle-of-attack accuracy and pneumatic lag can be adequately characterized and incorporated into a real-time algorithm.
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Category :
Languages : en
Pages : 1070
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Category : Science
Languages : en
Pages : 814
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 980
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 980
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Two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, historians, museum curators, journalists, and independent scholars. Explores various aspects of how NACA-NASA research took aeronautics from the subsonic to the hypersonic era.-publisher description.
Author: Robert G. Ferguson
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ISBN:
Category : Aeronautics
Languages : en
Pages : 312
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ISBN:
Category :
Languages : en
Pages : 180
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