44th AIAA Aerospace Sciences Meeting and Exhibit 2006
DOI: 10.2514/6.2006-1385
|View full text |Cite
|
Sign up to set email alerts
|

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

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2023
2023
2023
2023

Publication Types

Select...
1

Relationship

0
1

Authors

Journals

citations
Cited by 1 publication
(1 citation statement)
references
References 0 publications
0
1
0
Order By: Relevance
“…The available literature on this topic is mostly limited to NACA reports from the 1950s. Therewith, a group of the profesores and students at the Air University in Pakistan, recently published a couple of manuscripts regarding this topic [5][6]. They used CFD analysis to determine the ogivale profile of the pitot tube in order to achieve the desirable pressure coefficient for both regimes, subsonic and supersonic.…”
Section: Introductionmentioning
confidence: 99%
“…The available literature on this topic is mostly limited to NACA reports from the 1950s. Therewith, a group of the profesores and students at the Air University in Pakistan, recently published a couple of manuscripts regarding this topic [5][6]. They used CFD analysis to determine the ogivale profile of the pitot tube in order to achieve the desirable pressure coefficient for both regimes, subsonic and supersonic.…”
Section: Introductionmentioning
confidence: 99%