Leading-Edge Flow Sensing for Aerodynamic Parameter Estimation-Reference-Cited by-同舟云学术

Leading-Edge Flow Sensing for Aerodynamic Parameter Estimation

Author:

Saini Aditya¹,Gopalarathnam Ashok¹

Affiliation:

1. North Carolina State University, Raleigh, North Carolina 27695-7910

Funder

Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

Reference83 articles.

1. KumbruchH. “Pitot-Static Tubes for Determining the Velocity of Air,” NACA TM 303, Feb. 1925.

2. ThompsonF. L. “The Measurement of Air Speed in Airplanes,” NACA TN 616, Jan. 1937.

3. MitchellJ. L.PeckR. F. “An NACA Vane-Type Angle-of-Attack Indicator for Use at Subsonic and Supersonic Speeds,” NACA TN 3441, May 1955.

4. HaeringE. A. “Airdata Measurement and Calibration,” NASA Dryden Flight Research Center TM 104316, 1995.

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