![]() ![]() No low-effort one-liner comments, memes, or off-topic replies. The design results show that the HAWT blades with NACA 5513 airfoil taperless type with a radius of 0.9 m on the airfoil simulation produced a higher CL/CD value with 152.73 when 4. Answers must contain an explanation using engineering logic, and assertions of fact must be supported by links to credible sources.īe substantive. Racism, sexism, or any other form of bigotry will not be tolerated.ĭon't answer if you aren't knowledgeable. Then surface has been created using SolidWorks with appropriate dimension suitable for wind tunnel testing. All users are expected to behave with courtesy. Experimental Setup First NACA 2415 airfoil surface has been generated by using C++ programming language by applying basic airfoil surface equation. Mechanical, Electrical, Civil, Chemical, and Computer are reserved for technical questions only.Ĭareer must be used for all questions on career advice, salary, job market, etc.ĭiscussion can be used for general questions that apply to multiple disciplines, including some workplace topics.īe respectful to other users. Remember to flair your post.Īvoid questions that can easily be answered by searching on the internet. Post titles must be a question about engineering and provide context - be specific. Call for Engineers: Tell us about your job! (2020) New to AskEngineers? Read our subreddit rules and FAQ page before posting! Topic Filters ⇨ Exclude All Career Posts ![]()
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