<?xml version="1.0" encoding="UTF-8"?>
<doi_batch version="4.3.0" xmlns="http://www.crossref.org/doi_resources_schema/4.3.0" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.crossref.org/doi_resources_schema/4.3.0 http://www.crossref.org/schema/deposit/doi_resources4.3.0.xsd">
<head>
<doi_batch_id>ec9cbca6-a989-454b-bbaa-5e3d30824cab</doi_batch_id>
<depositor>
<name>beie</name>
<email_address>director@blueeyesintelligence.org</email_address>
</depositor>
</head>
<body>
<doi_citations>
<doi>10.35940/ijitee.C9812.13030224</doi>
<citation_list><citation key="ref0"><unstructured_citation>Anderson J.D., &quot;Fundamentals of Aerodynamics&quot;, McGraw-Hill, New York, NY, USA, 2007.</unstructured_citation></citation><citation key="ref1"><doi>10.37896/jxu14.6/312</doi><unstructured_citation>Subha, Rosy &amp; D'rozario, Anthony Mario &amp; Manojith, Sreeshin, &quot;Study on Various Types of Nose Cone Profiles at Supersonic Speed Through Analytical&quot;, Experimental And Numerical Simulation Methods. Journal of Xidian University. 14. 10.37896/Jxu14.6/312, 2020. https://doi.org/10.37896/jxu14.6/312</unstructured_citation></citation><citation key="ref2"><unstructured_citation>Yeshwanth, A. &amp; Senthiil, P.V. &quot;Nose cone design and analysis of an avion&quot;, International Journal of Pure and Applied Mathematics, 119. 15581-15588, 2018.</unstructured_citation></citation><citation key="ref3"><unstructured_citation>Kumar, P. Kiran. &quot;Analysis of nose cone of the missile.&quot; International Journal of Engineering Research and Applications, ISSN 2248-9622, 2020.</unstructured_citation></citation><citation key="ref4"><unstructured_citation>Rozario and Anthony Mario, &quot;Study on Various Types of Nose Cone Profiles at Supersonic Speed through Analytical, Experimental and Numerical Simulation Methods.&quot;</unstructured_citation></citation><citation key="ref5"><doi>10.2514/1.A33316</doi><unstructured_citation>Schinetsky P. A., B. T. Brooker, A. Treadway, S. M. Olcmen, S. E. Jones, &quot;Numerical and experimental analysis of projectile nose geometry&quot;, Journal of Spacecraft and Rockets, 52(5), 1515-1519, 2015. https://doi.org/10.2514/1.A33316</unstructured_citation></citation><citation key="ref6"><doi>10.2514/2.3189</doi><unstructured_citation>Foster N. F., G. S. Dulikravich, &quot;Three-dimensional aerodynamic shape optimization Using genetic and gradient search algorithms,&quot; Journal of Rockets and Spacecraft, 34(1), 36-42, 1997. https://doi.org/10.2514/2.3189</unstructured_citation></citation><citation key="ref7"><doi>10.2514/1.33826</doi><unstructured_citation>Deepak N. R., T. Ray, R. R. Russell, &quot;Evolutionary algorithm Shape Optimization of a Hypersonic Flight Experiment Nose Cone&quot;, Journal of Spacecraft and Rockets, 45(3), 2008. https://doi.org/10.2514/1.33826</unstructured_citation></citation><citation key="ref8"><doi>10.1115/IMECE2015-50264</doi><unstructured_citation>Ranjan R. R., D. V. Parmar, H. K. Raipuria, P. B. Singh, &quot;Innovative nose cone design of aircraft&quot;, ASME International Mechanical Engineering Congress and Exposition, Texas, USA, November 2015. https://doi.org/10.1115/IMECE2015-50264</unstructured_citation></citation><citation key="ref9"><unstructured_citation>Garry A., Crowell Sr, &quot;The Descriptive Geometry of Nose Cone&quot;, 1996.</unstructured_citation></citation><citation key="ref10"><unstructured_citation>Varma A. S., G. S. Sathyanarayana, &quot;CFD analysis of various nose profiles&quot;, International Journal of Aerospace and Mechanical Engineering, 3(3), 26-29, 2016.</unstructured_citation></citation><citation key="ref11"><unstructured_citation>Harish S., D. Hasen, V. Giridharan, &quot;Computational study on surface pressure distribution and base pressure distribution over parabolic series nose cone&quot;, Journal of Chemical and Pharmaceutical Sciences, 9(2), 0974-2115, 2016.</unstructured_citation></citation><citation key="ref12"><doi>10.35940/ijeat.B3560.129219</doi><unstructured_citation>Rafie, A. S. M., Magaidi, A. M., &amp; Marzuki, O. F. (2019). Aerodynamic Performance of Biomimicry Snake-Shaped Airfoil. In International Journal of Engineering and Advanced Technology (Vol. 9, Issue 2, pp. 3319-3323). https://doi.org/10.35940/ijeat.b3560.129219</unstructured_citation></citation><citation key="ref13"><doi>10.35940/ijitee.B6183.129219</doi><unstructured_citation>Mishra, N. K., Kumar, A. S., Ganesh, M., &amp; Rehman Alam, M. A. (2019). Design of Minimum Length Supersonic Nozzle using the Method of Characteristics. In International Journal of Innovative Technology and Exploring Engineering (Vol. 9, Issue 2, pp. 1370-1374). https://doi.org/10.35940/ijitee.b6183.129219</unstructured_citation></citation><citation key="ref14"><doi>10.35940/ijrte.E9862.038620</doi><unstructured_citation>P, D., Verma, A., Reddy, C. J., Suri S, J., &amp; M, V. (2020). Boundary Layer Control of Airfoil using Rotating Cylinder. In International Journal of Recent Technology and Engineering (IJRTE) (Vol. 8, Issue 6, pp. 4742-4750). https://doi.org/10.35940/ijrte.e9862.038620</unstructured_citation></citation><citation key="ref15"><doi>10.35940/ijeat.F1360.089620</doi><unstructured_citation>Shaheen, A., &amp; Sinha, A. D. (2020). Crash Analysis of Aircraft Nose Prototype. In International Journal of Engineering and Advanced Technology (Vol. 9, Issue 6, pp. 204-213). https://doi.org/10.35940/ijeat.f1360.089620</unstructured_citation></citation><citation key="ref16"><journal_title>In International Journal of Management and Humanities (Vol</journal_title><author>Pandey</author><cYear>2020</cYear><doi>10.35940/ijmh.j0973.0641020</doi><article_title>Real-time Forecasting of COVID-19 Prevalence in India using ARIMA Model</article_title><unstructured_citation>Pandey, S., &amp; Samanta, A. (2020). Real-time Forecasting of COVID-19 Prevalence in India using ARIMA Model. In International Journal of Management and Humanities (Vol. 4, Issue 10, pp. 78-83).</unstructured_citation></citation></citation_list>
</doi_citations>
</body>
</doi_batch>
