STUDENT ANALYSIS OF AIRCRAFT WINGS WITH VARIOUS CONDITIONS /
Salvato in:
| Autore principale: | |
|---|---|
| Ente Autore: | |
| Altri autori: | , , |
| Natura: | Libro |
| Lingua: | inglese |
| Pubblicazione: |
Dhaka :
AE DEPT MIST ,
C 2015 .
|
| Soggetti: | |
| Tags: |
Nessun Tag, puoi essere il primo ad aggiungerne!!
|
Documenti analoghi: STUDENT ANALYSIS OF AIRCRAFT WINGS WITH VARIOUS CONDITIONS /
- STRUCTURAL ANALYSIS OF AIR CRAFT WINGS WITH VARIOUS CONDITIONS /
- LARGE DEFECTION ANALYSIS OF AN AIRCRAFT WING WITH ELLIPTICAL LIFT DISTRIBUTION AT DIFFERENT FLIGHT CONDITION /
- PERFORMANCE OPTIMIZATION OF A VARIABLE GEOMETRICAL WING:ANALYSIS AND DESIGN OF MORPHING WING FOR UNMANNED AERIAL VEHICLE /
- DESIGN & FABRICATION OF WING CONTROLS,UNDERCARRIAGE AND SKIN OF HOME BUILT EXPERIMENTAL AIRCRAFT’’ MIST X-01’’ /
- PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /
- PROPERTIES OF NATURAL POLYMER MATRIX COMPOSITE WITH VARIOUS FIBER ORIENTATIONS /