- Bài trích
- Nhan đề: A method for nonlinear aeroelasticity trim and stability analysis of very flexible aircraft based on co-rotational theory /Wei Wang a,1 , Xiaoping Zhu b,2 , Zhou Zhou a,n,3 , Jingbo Duan
|
Tác giả CN
| Wang,Wei | |
Nhan đề
| A method for nonlinear aeroelasticity trim and stability analysis of very flexible aircraft based on co-rotational theory /Wei Wang a,1 , Xiaoping Zhu b,2 , Zhou Zhou a,n,3 , Jingbo Duan | |
Từ khóa tự do
| Nonlinear aeroelasticity | |
Từ khóa tự do
| Trim | |
Từ khóa tự do
| Very flexible aircraft | |
Nguồn trích
| Journal of fluids and structures2016-4
Số: 1
Tập: 62 |
| | 000 | 00000nab#a2200000ui#4500 |
|---|
| 001 | 14135 |
|---|
| 002 | 6 |
|---|
| 004 | F1ACFCD6-F512-46D6-9403-F5A405E48038 |
|---|
| 005 | 201706221438 |
|---|
| 008 | 081223s vm| vie |
|---|
| 009 | 1 0 |
|---|
| 039 | |y20170622144547|zcuonglv |
|---|
| 100 | |aWang,Wei |
|---|
| 245 | |aA method for nonlinear aeroelasticity trim and stability analysis of very flexible aircraft based on co-rotational theory /Wei Wang a,1 , Xiaoping Zhu b,2 , Zhou Zhou a,n,3 , Jingbo Duan |
|---|
| 653 | |aNonlinear aeroelasticity |
|---|
| 653 | |aTrim |
|---|
| 653 | |aVery flexible aircraft |
|---|
| 773 | |tJournal of fluids and structures|v62|i1|d2016-4 |
|---|
| 890 | |c1|a0|b0|d5 |
|---|
|
Không tìm thấy biểu ghi nào
|
|
|
|