1991
DOI: 10.2514/3.46039
|View full text |Cite
|
Sign up to set email alerts
|

Computed Euler flowfield for a transonic aircraft with stores

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
5
0

Year Published

1992
1992
2004
2004

Publication Types

Select...
7
1

Relationship

0
8

Authors

Journals

citations
Cited by 12 publications
(5 citation statements)
references
References 4 publications
0
5
0
Order By: Relevance
“…Newman and Baysal [72] employed a hybrid domain decomposition for the transonic flow over a wingpylon-finned store, Tu et al [79] used unstructured grids to study the flow over a wing-pylonstore configuration in the transonic and supersonic speed range, and Fox et al [57] analyzed the flow around an F-15E aircraft with finned stores with a grid embedding technique. All methods agreed well with experimental data.…”
Section: Transonic Flowmentioning
confidence: 99%
“…Newman and Baysal [72] employed a hybrid domain decomposition for the transonic flow over a wingpylon-finned store, Tu et al [79] used unstructured grids to study the flow over a wing-pylonstore configuration in the transonic and supersonic speed range, and Fox et al [57] analyzed the flow around an F-15E aircraft with finned stores with a grid embedding technique. All methods agreed well with experimental data.…”
Section: Transonic Flowmentioning
confidence: 99%
“…9, also from Ref. 19, where the Mach number contours on the surface of the F-15E loaded with a GBU-15, targeting pod, and centerline fuel tank are presented.…”
Section: Flow-field Incrementsmentioning
confidence: 99%
“…8, taken from Ref. 19, where the upwash and sidewash angle for the flow near the F-15E computed using the inviscid Euler equations for M = 0.98 are compared with the measurements made with a flow probe grid survey. The comparison is excellent.…”
Section: Flow-field Incrementsmentioning
confidence: 99%
See 1 more Smart Citation
“…CFD is not limited by the constraints of model complexity, scale, and support requirements that plague the wind tunnel when testing aerodynamic bodies in close proximity. The ability of CFD to accurately predict the loads and trajectories of stores in the flow field of a parent aircraft has been demonstrated by a number of investigators including Fox, et al, 1 Donegan and Fox, 2 and Nichols, et al 3 These studies indicate that CFD can provide meaningful insight into complex multi-body problems if care is taken to include the appropriate physical processes and geometrical detail. CFD also allows the analyst to look at the details of the flow field, adding insight that cannot be obtained from traditional wind tunnel tests.…”
Section: Introductionmentioning
confidence: 99%