Zobrazeno 1 - 10
of 25
pro vyhledávání: '"Charles M. Denegri"'
Publikováno v:
Journal of Aircraft. 58:236-243
Earlier work did not find any static stiffness nonlinearities in the F-16 wing structure, but suggested that dynamic nonlinearities may be present. Computational studies have demonstrated that smal...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::17b15581dca94a5512840ef36aae0f73
https://doi.org/10.2514/1.c035850
https://doi.org/10.2514/1.c035850
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::46ee03de0d1b68efc118380672842420
https://doi.org/10.2514/6.2019-2034.c1
https://doi.org/10.2514/6.2019-2034.c1
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f7fe505b7715db92fa7074062df8f079
https://doi.org/10.2514/6.2019-2034
https://doi.org/10.2514/6.2019-2034
Publikováno v:
Journal of Aircraft. 53:243-250
A well-known F-16 external store configuration was studied using a time-domain computational aeroelasticity code. The code used a medium-fidelity Euler flow solver coupled with a linear modal representation of the structure. A key feature of the code
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3de9a03658ec20ff17b329a93a2734ff
https://doi.org/10.2514/1.c033315
https://doi.org/10.2514/1.c033315
Publikováno v:
Journal of Aircraft. 50:1637-1645
F-16 testing revealed differences in limit-cycle oscillation response characteristics associated with subtle aerodynamic variations of the underwing missiles. Physical length differences between long and short missiles led to the accidental discovery
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::768ba6fe9c9630902cccd26a4cc2f7e6
https://doi.org/10.2514/1.c032216
https://doi.org/10.2514/1.c032216
Publikováno v:
Journal of Aircraft. 51:693-695
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::245f000543da67b38e0d127d1a8960d6
https://doi.org/10.2514/1.c032547
https://doi.org/10.2514/1.c032547
Publikováno v:
Journal of Aircraft. 46:1667-1672
A computational investigation of the flutter onset and limit cycle oscillation behavior of various F-16 fighter weapons and stores configurations is presented. A nonlinear harmonic balance compressible Reynolds-averaged Navier–Stokescomputational f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::acfff7be13b8ee553afc2de7266dc867
https://doi.org/10.2514/1.42352
https://doi.org/10.2514/1.42352
Publikováno v:
Journal of Aircraft. 42:500-508
Oscillatory wing response data were measured on an F-16C aircraft during limit-cycle-oscillation (LCO) testing of an external store configuration. The configuration tested exhibited typical LCO response in the transonic flight regime. Deformation cha
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f899b0e17b5e4a12f7e04498e478a8ce
https://doi.org/10.2514/1.1345
https://doi.org/10.2514/1.1345
Autor:
Michael R. Johnson, Charles M. Denegri
Publikováno v:
Journal of Aircraft. 40:194-203
A dynamic artificial neural network in the form of a multilayer perceptron with a delayed recurrent feedback connection is investigated to determine its ability to predict linear and nonlinear flutter response characteristics. Flight-test results sho
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b4b5b47a857d1dde0ad3132333a5ac9c
https://doi.org/10.2514/2.3075
https://doi.org/10.2514/2.3075
Autor:
Michael R. Johnson, Charles M. Denegri
Publikováno v:
Journal of Guidance, Control, and Dynamics. 24:887-895
A static arti cial neural network in the form of a multilayer perceptron is investigated to determine its ability to predict linear and nonlinear utter response characteristics. The network is developed and trained using linear utter analysis
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2c389812791e3b8c0cd3ce6dce418061
https://doi.org/10.2514/2.4824
https://doi.org/10.2514/2.4824