| Admissions | Accreditation | A to Z Degree Fields | Booksellers | Catalog | Colleges | Contact Us | Continents/States/Districts | Contracts | Distance Education | Emergency | Emergency Medicine | Examinations | Forms | Grants | Hostels | Honorary Doctorate degree | Human Services | Internet | Investment | Instructors | Login | Lecture | Librarians | Membership | Observers | Professional Examinations | Programs | Progress Report | Recommendations | Research Grants | Researchers | Students login | School | Search | Seminar | Study Center/Centre | Sponsorship | Tutoring | Thesis | Universities | Work counseling |
|
What should be the thrust of the aircraft engine you plan to manufacture: 50,000 pounds, 45,000 pounds, or 40,000 pounds?
How many engines will be attached to the aircraft you plan to manufacture? 2. Four or any other number. How much titanium is required to manufacture an aircraft engine with thrust of 50,000 pounds and dry weight of 4,100 kg (9,039 lb)? What are the length, width, height, fan diameter, dry weight, fan type, and other characteristics of aircraft engine you plan to manufacture? What are the details of components like compressor, combustors, and turbine of the aircraft engine you plan to manufacture? What should be the thrust-to-weight ratio of the aircraft you plan to manufacture? What are the two most important parameters that determine performance of an aircraft? The thrust-to-weight ratio (Thrust to Airplane Weight Ratio) and wing loading. What is the wing loading of the aircraft you plan to manufacture? In aerodynamics, wing loading is the loaded weight of the aircraft divided by the area of the wing. How does wing loading affect the performance of an aircraft? |