Numerical Predictions of Static-Pressure-Error Corrections for a Modified T-38C Aircraft-Reference-Cited by-同舟云学术

Numerical Predictions of Static-Pressure-Error Corrections for a Modified T-38C Aircraft

Published:2015-07 Issue:4 Volume:52 Page:1326-1335
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Reasor Daniel A.¹,Bhamidipati Keerti K.¹,Woolf Reagan K.¹

Affiliation:

1. U.S. Air Force, Edwards Air Force Base, California 93524

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032925

Reference27 articles.

1. “Installation and Inspection of Pitot-Static Pressure Systems,” U.S. Air Force MIL-P-26292C, Wright-Patterson AFB, 1969.

2. BhamidipatiK. K.LechniakJ. A.WoolfR. K. “T-38C Noseboom Pressure and Velocity Study Using Computational Fluid Dynamics,” U.S. Air Force Flight Test Center AFFTC-TIM-11-06, Edwards AFB, CA, 2012.

3. GraceyW. “Measurement of Static Pressure on Aircraft,” NACA Rept. 1364, 1956.

4. DeLeoR. V.HagenF. W. “Flight Calibration of Aircraft Static Pressure Systems,” Federal Aviation Agency, Systems Research and Development Service Rept. RD-66-3, Rosemount Engineering Co. Rept. 76431, Minneapolis, MN, 1966.

5. WuestW. “Pressure and Flow Measurement,” AGARD AG-160, Vol. 11, AGARD Flight Test Instrumentation Series, 1980.

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