Performance Characteristics of Flush Angle-of-Attack Measurement System Integrated on a Pitot Tube-Reference-Cited by-同舟云学术

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Performance Characteristics of Flush Angle-of-Attack Measurement System Integrated on a Pitot Tube

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
language:
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Author:

Masud Jehanzeb¹,Afgan Imran¹

Affiliation:

1. IAA, Air University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1077

Reference11 articles.

1. 1Garcy,W."MeasurementofAircraftSpeedandAltitude,"NASAReferencePublication1046,1980.

2. Computation of transonic aerodynamically compensating pilot tube

3. 5Schreier,S."TwoandThreeDimensionalSteady SupersonicFlow,"CompressibleFlow,Wiley,NewYork,1982,pp.133-200.

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical analysis of aerodynamic compensation pitot-static tube;Scientific Technical Review;2023

2. Bio-Inspired Air Data Sensing Probe for High Angles of Attack and Sideslip;53rd AIAA Aerospace Sciences Meeting;2015-01-03

3. Adjustment of Aerodynamic-Compensation Characteristics of a Pitot Tube by Rear-Body Shape Manipulation;Journal of Fluids Engineering;2010-03-01

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