Recomienda este artículo a tus amigos:
Comparison of Pitching Moments Produced by Plain Flaps and by Spoilers and Some Aerodynamic Characteristics of an NACA 23012 Airfoil With Various Types of Aileron Langley Aeronautical Laboratory
Precio
$ 21,99
sin IVA
Pedido desde almacén remoto
Entrega prevista 22 de jun. - 9 de jul.
Nuestros clientes opinan:
Añadir a tu lista de deseos de iMusic
Comparison of Pitching Moments Produced by Plain Flaps and by Spoilers and Some Aerodynamic Characteristics of an NACA 23012 Airfoil With Various Types of Aileron
Langley Aeronautical Laboratory
| Medios de comunicación | Libros Paperback Book (Libro con tapa blanda y lomo encolado) |
| Publicado | 9 de septiembre de 2021 |
| ISBN13 | 9781014112767 |
| Editores | Hassell Street Press |
| Páginas | 26 |
| Dimensiones | 150 × 220 × 10 mm · 49 g |
Mas por Langley Aeronautical Laboratory
Mostrar todo
![Cover for Langley Aeronautical Laboratory · Airfoil-contour Modifications Based on [epsilon]-curve Method of Calculating Pressure Distribution (Paperback Book) (2021)](https://imusic.b-cdn.net/images/item/original/172/9781015153172.jpg?langley-aeronautical-laboratory-2021-airfoil-contour-modifications-based-on-epsilon-curve-method-of-calculating-pressure-distribution-paperback-book&class=scaled&v=1646960123)
Ver todo de Langley Aeronautical Laboratory ( Ej. Paperback Book , Hardcover Book y Book )