Authors Index
| Author | Manuscripts |
|
Hiroshi Nakamura
IHI |
84 Consideration of life prediction model for ceramic matrix composite(CMC) with cooling hole |
|
Ömer Namdar
|
113 Crack bridging effect in hybrid reinforced fuselage structure |
|
J.C. Newman, Jr.
Mississippi State University, USA |
1 Fatigue Crack Growth on Several Materials under Single Spike Overloads and Aircraft Spectra |
|
Vesa Nieminen
|
85 Modal testing of vertical tail of F/A-18 Hornet 95 VIBFAT – Vibration-Induced Fatigue life estimation of the Vertical Tail of the F/A-18 aircraft using virtual sensing |
|
Daisuke Nishida
Kawasaki Heavy Industries, Ltd |
130 Optimal design and static load testing of tow-steered aircraft fuselage frames |
|
Marv Nuss
Consultant |
11 Probabilistic damage tolerance analysis using adaptive multiple importance sampling |
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