Estimation of aircraft dynamic parameters using Euler computations and comparison with flight-test data

S.J. Hulshoff; J.A. Mulder; H.W.M. Hoeijmakers

doi:10.2514/6.1996-3416

Estimation of aircraft dynamic parameters using Euler computations and comparison with flight-test data

S.J. Hulshoff, J.A. Mulder, H.W.M. Hoeijmakers

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic › peer-review

Abstract

An Euler method for the computation of steady and unsteady flows is applied to the prediction of longitudinal dynamic parameters for a full aircraft configuration. Both a simplified wing-tail representation and a detailed geometric representation are considered. In order to evaluate the accuracy of the approach, computed values are directly compared with flight-test data. The results reveal the importance of considering detailed models of the complete configuration for the accurate determination of dynamic response.

Original language	English
Title of host publication	21st Atmospheric Flight Mechanics Conference 1996
Subtitle of host publication	29 July 1996 - 31 July 1996, San Diego, CA, U.S.A.
Place of Publication	Reston, VA
Publisher	Aerospace Research Central
Number of pages	12
DOIs	https://doi.org/10.2514/6.1996-3416
Publication status	Published - 1996
Externally published	Yes
Event	21st Atmospheric Flight Mechanics Conference 1996 - San Diego, United States Duration: 29 Jul 1996 → 31 Jul 1996 Conference number: 21

Publication series

Name	AIAA Meeting Paper
Publisher	Aerospace Research Central
Number	96-3416
ISSN (Print)	0146-3705

Conference

Conference	21st Atmospheric Flight Mechanics Conference 1996
Country/Territory	United States
City	San Diego
Period	29/07/96 → 31/07/96

Access to Document

10.2514/6.1996-3416

Cite this

Hulshoff, S. J., Mulder, J. A., & Hoeijmakers, H. W. M. (1996). Estimation of aircraft dynamic parameters using Euler computations and comparison with flight-test data. In 21st Atmospheric Flight Mechanics Conference 1996: 29 July 1996 - 31 July 1996, San Diego, CA, U.S.A. (AIAA Meeting Paper; No. 96-3416). Aerospace Research Central. https://doi.org/10.2514/6.1996-3416

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title = "Estimation of aircraft dynamic parameters using Euler computations and comparison with flight-test data",

abstract = "An Euler method for the computation of steady and unsteady flows is applied to the prediction of longitudinal dynamic parameters for a full aircraft configuration. Both a simplified wing-tail representation and a detailed geometric representation are considered. In order to evaluate the accuracy of the approach, computed values are directly compared with flight-test data. The results reveal the importance of considering detailed models of the complete configuration for the accurate determination of dynamic response.",

author = "S.J. Hulshoff and J.A. Mulder and H.W.M. Hoeijmakers",

year = "1996",

doi = "10.2514/6.1996-3416",

language = "English",

series = "AIAA Meeting Paper",

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Hulshoff, SJ, Mulder, JA & Hoeijmakers, HWM 1996, Estimation of aircraft dynamic parameters using Euler computations and comparison with flight-test data. in 21st Atmospheric Flight Mechanics Conference 1996: 29 July 1996 - 31 July 1996, San Diego, CA, U.S.A.. AIAA Meeting Paper, no. 96-3416, Aerospace Research Central, Reston, VA, 21st Atmospheric Flight Mechanics Conference 1996, San Diego, California, United States, 29/07/96. https://doi.org/10.2514/6.1996-3416

Estimation of aircraft dynamic parameters using Euler computations and comparison with flight-test data. / Hulshoff, S.J.; Mulder, J.A.; Hoeijmakers, H.W.M.
21st Atmospheric Flight Mechanics Conference 1996: 29 July 1996 - 31 July 1996, San Diego, CA, U.S.A.. Reston, VA: Aerospace Research Central, 1996. (AIAA Meeting Paper; No. 96-3416).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic › peer-review

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AU - Hoeijmakers, H.W.M.

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PY - 1996

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N2 - An Euler method for the computation of steady and unsteady flows is applied to the prediction of longitudinal dynamic parameters for a full aircraft configuration. Both a simplified wing-tail representation and a detailed geometric representation are considered. In order to evaluate the accuracy of the approach, computed values are directly compared with flight-test data. The results reveal the importance of considering detailed models of the complete configuration for the accurate determination of dynamic response.

AB - An Euler method for the computation of steady and unsteady flows is applied to the prediction of longitudinal dynamic parameters for a full aircraft configuration. Both a simplified wing-tail representation and a detailed geometric representation are considered. In order to evaluate the accuracy of the approach, computed values are directly compared with flight-test data. The results reveal the importance of considering detailed models of the complete configuration for the accurate determination of dynamic response.

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Y2 - 29 July 1996 through 31 July 1996

ER -

Estimation of aircraft dynamic parameters using Euler computations and comparison with flight-test data

Abstract

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Conference

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