TY - GEN
T1 - Drag Decomposition of Full Aircraft Configurations Using Partial-Pressure Fields
AU - Hart, Pierce L.
AU - Axten, Christopher J.
AU - Maughmer, Mark D.
AU - Schmitz, Sven
N1 - Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2022
Y1 - 2022
N2 - The development of Partial-Pressure Field theory, ("Drag Decomposition Using Partial-Pressure Fields in the Compressible Navier-Stokes Equations", AIAA Journal, Vol. 57, No. 5, 2019, pp. 2030-2038), and the application of the theoretical concept to conditions relevant to commercial transport aircraft, operating in both the subsonic and transonic regime, ("Application of Partial-Pressure Field Drag Decomposition to the ONERA M6 Wing", Vol. 60, No. 5, 2022 pp. 2941-2951), has shown promise as a complement to classical far-field methods within computational fluid dynamics. In the present work, the NASA Common Research Model is simulated under transonic flow conditions to demonstrate the applicability of partial-pressure fields to drag decomposition of full aircraft configurations, with results of the near-field drag decomposition compared to classical far-field methods.
AB - The development of Partial-Pressure Field theory, ("Drag Decomposition Using Partial-Pressure Fields in the Compressible Navier-Stokes Equations", AIAA Journal, Vol. 57, No. 5, 2019, pp. 2030-2038), and the application of the theoretical concept to conditions relevant to commercial transport aircraft, operating in both the subsonic and transonic regime, ("Application of Partial-Pressure Field Drag Decomposition to the ONERA M6 Wing", Vol. 60, No. 5, 2022 pp. 2941-2951), has shown promise as a complement to classical far-field methods within computational fluid dynamics. In the present work, the NASA Common Research Model is simulated under transonic flow conditions to demonstrate the applicability of partial-pressure fields to drag decomposition of full aircraft configurations, with results of the near-field drag decomposition compared to classical far-field methods.
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U2 - 10.2514/6.2022-3885
DO - 10.2514/6.2022-3885
M3 - Conference contribution
AN - SCOPUS:85135370883
SN - 9781624106354
T3 - AIAA AVIATION 2022 Forum
BT - AIAA AVIATION 2022 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA AVIATION 2022 Forum
Y2 - 27 June 2022 through 1 July 2022
ER -