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Development of a computer program to obtain ordinates for naca-6 and 6a-series airfoils
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ladson, C. L. Brooks Jr., C. W. |
| Copyright Year | 1974 |
| Description | A computer program was developed to produce the ordinates for airfoils of any thickness, thickness distribution, or camber in the NACA 6- and 6A-series. For the 6-series and for all but the leading edge of the 6A-series, agreement between the ordinates obtained from the new program and previously published values is generally within .00005 chord. Near the leading edge of the 6A-series airfoils, differences up to .00035 chord are found. |
| File Size | 4355057 |
| Page Count | 106 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740025318 |
| Archival Resource Key | ark:/13960/t6k11vd7j |
| Language | English |
| Publisher Date | 1974-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Numerical Analysis Aerodynamic Configurations Airfoil Profiles Rotor Aerodynamics Computer Aided Design Rotary Wings Wing Camber Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
