Several Methods for Aerodynamic Reduction of Static-pressure Sensing Errors for Aircraft at Subsonic, Near-sonic, and Low Supersonic Speeds

Several Methods for Aerodynamic Reduction of Static-pressure Sensing Errors for Aircraft at Subsonic, Near-sonic, and Low Supersonic Speeds
Author: Virgil S. Ritchie
Publisher:
Total Pages: 36
Release: 1959
Genre: Aerodynamics
ISBN:

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Tests were conducted in transonic wind tunnels to investigate and verify experimentally methods for aerodynamically reducing errors due to sensor position, bow-wave passage, and angle of attack. The results indicated that aerodynamics devices of simple design may be employed to reduce errors in sensing static pressure to less than 0.5 percent at Mach numbers from about 0.40 to 1.15.

NASA Technical Report

NASA Technical Report
Author:
Publisher:
Total Pages: 36
Release: 1959
Genre: Aerodynamics
ISBN:

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Index of NASA Technical Publications

Index of NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
Total Pages: 448
Release: 1960
Genre: Aeronautics
ISBN:

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NASA Reference Publication

NASA Reference Publication
Author:
Publisher:
Total Pages: 852
Release: 1977
Genre: Astronautics
ISBN:

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NASA Technical Note

NASA Technical Note
Author:
Publisher:
Total Pages: 616
Release: 1975
Genre:
ISBN:

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