Investigation of the effects of angle of attack and tail deflection angle on the controlling tail flow field-Reference-Cited by-同舟云学术

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Investigation of the effects of angle of attack and tail deflection angle on the controlling tail flow field

Published:2020-10-19 Issue:4 Volume:3 Page:309-326
ISSN:2523-3947
Container-title:Aerospace Systems
language:en
Short-container-title:AS

Author:

Mokhtari Ali,Shahrian Azadeh,Langroodi Pooya Javadpoor,Ghodrat Maryam^ORCID

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Computers in Earth Sciences,Mechanical Engineering,Social Sciences (miscellaneous),Aerospace Engineering,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42401-020-00063-w.pdf

Reference62 articles.

1. Davari A, Dulabi MH, Soltani MR (2009) Impact of body on the tail surface flowfield at high incidences. J Aerosp Sci Technol 6(1):25–35

2. Elsenaar A, Hjelmberg L, Bütefisch KA, Bannink WJ (1988) The international vortex flow experiment. AGARD-CP 437(1):1–23

3. Wagner B, Hitzel S, Schmatz MA, Schwarz W, Hilgenstock A, Scherr S (1988) Status of CFD validation on the vortex flow experiment. AGARD-CP 437(1):1–10

4. Hoeijmakers HWM (1991) Modelling and numerical simulation of vortex flow in aerodynamics. AGARD-CP 494:1–46

5. Luckring JM (1991) Recent progress in computational vortex-flow aerodynamics. AGARDCP 494:6–21

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