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Main rotor downwash effect on separation characteristics of external stores
Date
2017-01-01
Author
Kapulu, Ozge
Tekinalp, Ozan
Metadata
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Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
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A proper simulation code developed to predict the behavior of stores after being released from a helicopter is presented. The effect of various inflow models on the collision of the store with the helicopter body is given. Also given is the effect of inflow model on the trajectory of the unguided missile launced from the helicopter. It is shown that the simulation code can predict unsafe cases and a useful analysis tool to determine critical flight conditions before carrying out actual flight tests.
URI
https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85088409582&origin=inward
https://hdl.handle.net/11511/107107
DOI
https://doi.org/10.2514/6.2017-1864
Conference Name
AIAA Atmospheric Flight Mechanics Conference, 2017
Collections
Department of Aerospace Engineering, Conference / Seminar
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BibTeX
O. Kapulu and O. Tekinalp, “Main rotor downwash effect on separation characteristics of external stores,” presented at the AIAA Atmospheric Flight Mechanics Conference, 2017, Colorado, Amerika Birleşik Devletleri, 2017, Accessed: 00, 2023. [Online]. Available: https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85088409582&origin=inward.
