{"id":34713,"date":"2024-10-11T15:50:16","date_gmt":"2024-10-11T15:50:16","guid":{"rendered":"https:\/\/www.writemyessays.app\/blog\/questions\/2-1-narrated-presentation-assignment-aircraft-assignment-airfoils-research-physical-laws\/"},"modified":"2024-10-11T15:50:16","modified_gmt":"2024-10-11T15:50:16","slug":"2-1-narrated-presentation-assignment-aircraft-assignment-airfoils-research-physical-laws","status":"publish","type":"questions","link":"https:\/\/www.writemyessays.app\/blog\/questions\/2-1-narrated-presentation-assignment-aircraft-assignment-airfoils-research-physical-laws\/","title":{"rendered":"2.1 Narrated Presentation Assignment: Aircraft Assignment, Airfoils Research, & Physical Laws"},"content":{"rendered":"

Overview<\/span><\/span><\/h3>\n

For this assignment, your instructor will assign a propeller-driven, single-engine, general aviation aircraft. You will research airfoils, apply physical laws concepts, and create a narrated presentation. You are expected to present your information as if teaching the concepts to someone who is not a pilot and is not familiar with aviation. These assignments allow you to build on our professional abilities to create and present college-level presentations that we would be proud to take into our prospective industries.<\/p>\n

Details<\/span><\/span><\/h3>\n

Refer to <\/span>ASCI 309 2.1 Assignment Lifts and Airfoils (DOCX)<\/b><\/a> <\/span><\/span><\/a><\/span>for the requirements of this assignment.<\/p>\n

 All provided answers must exemplify the concepts with specific numbers\/values for your aircraft. For example, we are not looking for the stall speed as given in the POH or on Wikipedia; we want to see how you derived a calculated stall speed based on your airfoil data, the particulars of your selected aircraft, and the application of the lift equation. Therefore, you must research additional information and\/or use your formula knowledge from this week’s readings to derive all the variables necessary to solve the lift equation.<\/p>\n

As a starting point and the minimum content to cover, a shortlist of considerations and discussion points are provided below and can be directly copied into your presentation:<\/p>\n

    \n
  1. Main airfoil for your assigned aircraft\n
      \n
    1. Stall AOA and associated CLmax<\/sub><\/li>\n
    2. Zero-lift AOA<\/li>\n
    3. Comparison of your main airfoil to a symmetric airfoil<\/li>\n<\/ol>\n<\/li>\n
    4. Resultant attribute discussions for your assigned aircraft\n
        \n
      1. Calculated stall speed.<\/li>\n
      2. How does lift change with airspeed if a constant AOA and altitude are held? (provide specific examples)<\/li>\n
      3. How does lift change with altitude if a constant AOA and airspeed are held? (provide specific examples)<\/li>\n
      4. How do the required CL and AOA for your specific aircraft (at a specific weight) change with changes in airspeed? (provide specific examples)<\/li>\n
      5. What happens if the required CL is larger than CLmax <\/span><\/sub>of your airfoil, and what speed regime is usually associated with that condition? Compare your main airfoil to a symmetric airfoil.<\/li>\n<\/ol>\n<\/li>\n<\/ol>\n

        The key to answering some questions is to provide specific calculation examples for your aircraft<\/strong> <\/span>that showcase the points made. You could do so in various forms, including self-generated tables and graphs or comparisons of key cases (e.g., comparing a low, medium, and high altitude case). You will notice that all such calculations are ultimately based on repeated but different applications of the lift equation. Therefore, to apply the lift equation, a couple of aspects about your aircraft have to be known (i.e., researched) or assumed (i.e., detailed in your explanations). These parameters include:<\/p>\n