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About Tables of Properties of Airfoil Polynomials - NASA Technical Reports
This monograph provides an extensive list of formulas for airfoil . u4(a:) : 1 -- 4x —— 12x2 + 8:63 + 161134 and x4 :2 1%(6210 -— 4111 + 4212 —— U3 + 114).
Detailed Information
| Author: | Unknown |
|---|---|
| Publication Year: | 2004 |
| Pages: | 21 |
| Language: | English |
| File Size: | 0.83 |
| Format: | |
| Price: | FREE |
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