Wind-Tunnel Investigation of a General-Aviation Differential Pressure Angle-of-Attack Probe
Author:
Affiliation:
1. Aerospace Engineering Department, U.S. Naval Academy, Annapolis, Maryland 21402
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032174
Reference4 articles.
1. GraceyW. “Summary of Methods of Measuring Angle of Attack on Aircraft,” NACA TN-4351, Aug. 1958.
2. ArendD. J.SaundersJ. D. “An Experimental Evaluation of the Performance of Two Combination Pitot Pressure Probes,” NASA TP-2009-215632M, Oct. 2009.
3. Fuel Efficiency of Small Aircraft
4. Flight Determination of Partial-Span-Flap Parasite Drag With Flap Deflection
Cited by 2 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. Chord and Flap Effects on a Differential Pressure Angle-of-Attack Probe;Journal of Aircraft;2019-01
2. Low-Cost Accurate Angle-of-Attack System;Journal of Aircraft;2018-03
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