Loading...
Please wait, while we are loading the content...
Similar Documents
Simplified aerodynamic analysis of the cyclogiro rotating wing system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1930 |
| Description | A simplified aerodynamic theory of the cyclogiro rotating wing is presented herein. In addition, examples have been calculated showing the effect on the rotor characteristics of varying the design parameters of the rotor. A performance prediction, on the basis of the theory here developed, is appended, showing the performance to be expected of a machine employing this system of sustentation. The aerodynamic principles of the cyclogiro are sound; hovering flight, vertical climb, and a reasonable forward speed may be obtained with a normal expenditure of power. Auto rotation in a gliding descent is available in the event of a power-plant failure. |
| File Size | 909567 |
| Page Count | 29 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930081369 |
| Archival Resource Key | ark:/13960/t4nk6j98f |
| Language | English |
| Publisher Date | 1930-01-01 |
| Access Restriction | Open |
| Subject Keyword | Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
