Name: Development of a Flush Airdata Sensing System on a Sharp-Nosed Vehicle for Flight at Mach 3 to 8 (en Inglés)
Price: 62197.00 COP
Availability: InStock
Author: Davis, Mark C. ; Nasa Technical Reports Server (Ntrs) ; Et Al
ISBN: 9781287286400

portada Development of a Flush Airdata Sensing System on a Sharp-Nosed Vehicle for Flight at Mach 3 to 8 (en Inglés)

Development of a Flush Airdata Sensing System on a Sharp-Nosed Vehicle for Flight at Mach 3 to 8 (en Inglés)

Formato

Libro Físico

Autor

Nasa Technical Reports Server (Ntrs)

Mark C. Davis

Editorial

Bibliogov

Idioma

Inglés

N° páginas

Encuadernación

Tapa Blanda

Dimensiones

24.6 x 18.9 x 0.1 cm

Peso

0.06 kg.

ISBN13

9781287286400

Categorías

Política y gobierno

Development of a Flush Airdata Sensing System on a Sharp-Nosed Vehicle for Flight at Mach 3 to 8 (en Inglés)

Nasa Technical Reports Server (Ntrs) (Autor) · Mark C. Davis (Autor) · Bibliogov · Tapa Blanda

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Reseña del libro "Development of a Flush Airdata Sensing System on a Sharp-Nosed Vehicle for Flight at Mach 3 to 8 (en Inglés)"

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 Mach 3-8 and at -6 deg - 12 deg angle of attack. 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 the 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.