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INTERNATIONAL JOURNAL OF NOVEL RESEARCH AND DEVELOPMENT International Peer Reviewed & Refereed Journals, Open Access Journal ISSN Approved Journal No: 2456-4184 | Impact factor: 8.76 | ESTD Year: 2016 Scholarly open access journals, Peer-reviewed, and Refereed Journals, Impact factor 8.76 (Calculate by google scholar and Semantic Scholar | AI-Powered Research Tool) , Multidisciplinary, Monthly, Indexing in all major database & Metadata, Citation Generator, Digital Object Identifier(DOI) |
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| Paper Title: | COMPUTATIONAL INVESTIGATION ON SLOTTED- SPLIT FLAP |
| Authors Name: | Mohan Prasath E , Kesavan M , Muthumari T |
| Download E-Certificate: | Download |
| Author Reg. ID: |
IJNRD_206395
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| Published Paper Id: | IJNRD2310049 |
| Published In: | Volume 8 Issue 10, October-2023 |
| DOI: | |
| Abstract: | Airfoil have number of questions must be answered before further development of the new transport aircraft design is approved. The manufacturer needs to knows; it can easily recoup their initial investment. The airline will order this new product only if it can expand its market, reduce costs and increase its revenue. The passenger wants a low-ticket price and high comfort. Society as a whole wants this new technology to improve the economy while protecting the environment. Most often, the camber is designed to increase the lift coefficient rather than decrease the drag coefficient. It is also helpful to shape the wing fold so that the tip will stall more slowly than the root. In unforeseen circumstances, this spin delay may allow the pilot to maintain control of the aircraft. A rounded airfoil has a virtually limitless range of possible designs, which is a fantastic tool in the aerodynamic engineer's toolbox. Practically, however, there is a finite number of common forms from which to choose if good data are available. The best choice depends on the type of aircraft and largely on the speed of the air flow. In this article, a special model for the skirt is proposed. The main goal of the model is to increase the efficiency of take-off of aircraft and to increase the efficiency of maneuvers during flight. |
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| Cite Article: | "COMPUTATIONAL INVESTIGATION ON SLOTTED- SPLIT FLAP", International Journal of Novel Research and Development (www.ijnrd.org), ISSN:2456-4184, Vol.8, Issue 10, page no.a428-a435, October-2023, Available :http://www.ijnrd.org/papers/IJNRD2310049.pdf |
| Downloads: | 000118767 |
| ISSN: |
2456-4184 | IMPACT FACTOR: 8.76 Calculated By Google Scholar| ESTD YEAR: 2016 An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 8.76 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator |
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Published Paper ID:IJNRD2310049 Registration ID: 206395 Published In: Volume 8 Issue 10, October-2023 DOI (Digital Object Identifier): Page No: a428-a435 Country: Erode, Tamil Nadu, India Research Area: Engineering Publisher : IJ Publication Published Paper URL : https://www.ijnrd.org/viewpaperforall?paper=IJNRD2310049 Published Paper PDF: https://www.ijnrd.org/papers/IJNRD2310049 |
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ISSN: 2456-4184
Impact Factor: 8.76 and ISSN APPROVED
Journal Starting Year (ESTD) : 2016
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