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Exploration of the Degree of Flow Field Congruency in the Integrated Mathematical Model of Subsonic Air Intake and Axial Flow Compressor.

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Bibliographic Details
Title: Exploration of the Degree of Flow Field Congruency in the Integrated Mathematical Model of Subsonic Air Intake and Axial Flow Compressor.
Authors: Yogesh, T. V.1, Nidamarty, Laasya P.1, Ramanamurty, S. V.1, Panigrahi, S. K.2 panigrahi.sk@gmail.com
Source: International Journal of Aeronautical & Space Sciences. Mar2026, Vol. 27 Issue 2, p1053-1064. 12p.
Database: Academic Search Ultimate
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Description
ISSN:2093274X
DOI:10.1007/s42405-025-01013-6