TIMMER W A.An overview of NACA 6-digit airfoil se-ries characteristics with reference to airfoils for largewind turbine blades. AIAA Paper2009-268 .Timmer, W.A., ―An Overview of NACA 6-digit airfoil series characteristics with reference to airfoils for large wind turbine blades‖, AIAA 2009...
UIUC Airfoil Data Sitem-selig.ae.illinois.edu/ads/coord_database.html 如果有画好的升力/阻力...
NACA 4 digit airfoils NACA 5 digit airfoils NACA 6 series airfoils Airfoils A to Z A a18 to avistar (88) B b29root to bw3 (22) C c141a to curtisc72 (40) D dae11 to du861372 (28) E e1098 to esa40 (209) F falcon to fxs21158 (121) G geminism to gu255118 (419) H hh...
不但可生成 NACA 4-digit，5-digit，6-digit翼型，还可生成Joukovsky 翼型，TsAGI B series翼型等一...
NACA Four-Digit Series:The first family of airfoils designed using this approach became known as the NACA Four-Digit Series. The first digit specifies the maximum camber (m) in percentage of the chord (airfoil length), the second indicates the position of the maximum camber (p) in tenths of...
Information is presented with which ordinates can be easily obtained for any thickness from 2 to 21 percent chord for NACA 63-, 64-, and 65-series airfoil sections and from 2 to 15 percent chord for NACA 63A-, 64-A, series airfoil sections. In addition, data required for estimation of...
Comparison of NACA 6-series and 4-digit airfoils for Darrieus wind turbines The aerodynamic efficiency of Darrieus wind turbines as effected by blade airfoil geometry was investigated. Analysis was limited to curved-bladed machines... P.G.,MIGLIORE - 《Journal of Energy》 被引量: 36发表: 1983...
I hope this information helps you learn more about NACA airfoil profiles. If you want to see some examples of NACA airfoils, you can use my graphic art tool to generate some images for you. Just type #graphic_art(“NACA xxxx”) where xxxx is the four-digit code of the airfoil you wan...
NACA0012 is one of the respective 4-digit series airfoils with a wide range of applications in the aeronautics and the turbomachinery sector, focused on vertical and horizontal stabilizer configurations. This is a symmetric airfoil with the maximum thickness distribution at 0.12c from the leading ...
1. Report'-No. NASA TM X-3284 2. GovarnmentAcc_sion No. 3. Recipient%CatalogNo. 4, Title and Subtitle '" DEVELOPMENT OF A COMPUTER PROGRAM TO OBTAIN ORDINATES FOR NACA 4-DIGIT, 4-DIGIT MODIFIED, 5-DIGIT_ AND 16-SERIES AIRFOILS 5,"Report Date November 1975 '' 6 PerforminOgrgani...