Zobrazeno 1 - 10
of 46
pro vyhledávání: '"B. H. K. Lee"'
Autor:
B. H. K. Lee
Publikováno v:
Journal of Aircraft. 47:732-736
T HE new generation of stores to be used on the F-22 and joint strike fighter (JSF) are designed as efficiently packaged, small, highly lethal minimissiles. Because of their lighter weights and smaller moments of inertia, these small smart bombs (SSB
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2588f490ed1da976ef6477c1244aec88
https://doi.org/10.2514/1.46684
https://doi.org/10.2514/1.46684
Publikováno v:
Journal of Aircraft. 38:17-21
In Part 1 the variations of the mean and rms normal force, bending and torsional moment coefficients on the vertical fin of an F/A-18 aircraft for different orientations and Mach numbers were examined by integrating the measured pressure differences
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3b3a42258d6e6a5e63542590c15c8c0b
https://doi.org/10.2514/2.2755
https://doi.org/10.2514/2.2755
Autor:
B. H. K. Lee
Publikováno v:
Journal of Aircraft. 47:1064-1066
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::42694c543de68797dc7940d4525fb332
https://doi.org/10.2514/1.46127
https://doi.org/10.2514/1.46127
Autor:
B. H. K. Lee
Publikováno v:
Journal of Aircraft. 47:343-345
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::814a6414fda276fb867db753cbcd9f75
https://doi.org/10.2514/1.45898
https://doi.org/10.2514/1.45898
Autor:
S. Marineau-Mes, B. H. K. Lee
Publikováno v:
Journal of Aircraft. 35:295-300
The pressure difference across the wing and leading-edge extension (LEX) of a rigid 6% scale model of an F/A-18 was measured, and the integrated static and rms loads were computed. The total loads on the aircraft were obtained using a sting-mounted b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1d19b7aadbec6c0b430976eec3fcfe11
https://doi.org/10.2514/2.2299
https://doi.org/10.2514/2.2299
Autor:
B. H. K. Lee, Y. S. Wong
Publikováno v:
Journal of Aircraft. 35:165-168
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c83a2d2ffbfc34c513175e3b6cc1090d
https://doi.org/10.2514/2.2280
https://doi.org/10.2514/2.2280
Autor:
B. H. K. Lee, D. E. Bean
Publikováno v:
Journal of Aircraft. 32:1351-1358
A method to predict full-scale buffet of the F/A-18 vertical tail using measurements taken on a rigid windtunnel model is presented. Tests were performed on a rigid 6% scale F/A-18 in the 1.5-m trisonic blowdown wind tunnel at the National Research C
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c1b17316bf2f67ea87fa072b165dfe71
https://doi.org/10.2514/3.46885
https://doi.org/10.2514/3.46885
Publikováno v:
Journal of Fluids and Structures. 9:175-193
A two-dimensional airfoil with either a bilinear or cubic structural nonlinearity in pitch, and subject to incompressible flow has been analysed; the aerodynamic forces on the airfoil are evaluated using Wagner's function. The resulting equations are
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cf6c31c253899b58d91535a2da15eb29
https://doi.org/10.1006/jfls.1995.1009
https://doi.org/10.1006/jfls.1995.1009
Publikováno v:
Journal of Aircraft. 31:1395-1401
A two-dimensiona l airfoil with a free-play nonlinearity in pitch subject to incompressibl e flow has been analyzed. The aerodynamic forces on the airfoil were evaluated using Wagner's function and the resulting equations integrated numerically to gi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bc364be02180c89c7b28b380668b7fa7
https://doi.org/10.2514/3.46664
https://doi.org/10.2514/3.46664
Publikováno v:
Journal of Aircraft. 31:862-867
The aim of this investigation is to provide a better understanding of the structure of the flowfield on the wing upper surface of an F/A-18 at high angles of attack. Time-averaged and rms pressure distributions were determined for different angles of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::107cd96436e289afc9674348e71b1bc6
https://doi.org/10.2514/3.46572
https://doi.org/10.2514/3.46572