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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
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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 |
![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)
