Novel Aerodynamic Compensation Pitot - Static Tube for Application in Subsonic and Supersonic Flight Regimes-Reference-Cited by-同舟云学术

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Novel Aerodynamic Compensation Pitot - Static Tube for Application in Subsonic and Supersonic Flight Regimes

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Latif Adnan¹,Masud Jehanzeb¹,Sheikh Shakil¹,Parvez Khalid¹,Qazi Omar¹,Qureshi Humayun¹

Affiliation:

1. National University of Sciences & Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-1385

Reference7 articles.

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

2. 2Letko, W. "Investigation of the Fuselage Interference on a Pitot-Static Tube Extending Forward From the Nose of the Fuselage,"NACA-TN-1496,1947.

3. 4FLUENT,ComputationalFluidDynamicsSoftwarePackage,Ver.6.2.16,FluentInc,Lebanon,NH,2004.

4. 6FLUENT,ComputationalFluidDynamicsSoftwarePackageUserGuide,Ver.6.2.16,FluentInc,Lebanon,NH,2004.

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

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