Posted: February 10th, 2023

This is for the Cirrus SR22 aircraft For your independent project, create an ins

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This is for the Cirrus SR22 aircraft
For your independent project, create an instructional presentation. Create a V-G diagram specific to your aircraft at a selected weight and atmospheric condition and explain how the V-G diagram can be utilized to identify specific maneuvering parameters. For inputs on how the V-G diagram is developed, read through Chapter 11 in the Flight Theory and Aerodynamics textbook.
At a minimum cover the following aspects:
Positive and negative limiting load factor (i.e., the maximum G allowed for your aircraft)
Stall speeds at 1, 2, 3, and so on G up to the maximum positive G (at your selected weight)
Ultimate load factor (ULF)
Positive ultimate load (i.e., the actual force [lbs]) at the selected weight
Maneuvering speed
The bank angle associated with the positive limiting load factor
For the specific maneuvering speed of your aircraft identified above, explain how to numerically find (provide the specific example and values) the associated turn rate and radius utilizing both of the following methods:
Rate and radius formula
The turn performance diagram (Figure 2.29 in Aerodynamics for Naval Aviators, Hurt, 1965, p.179 or the Constant altitude turn performance diagram/figure in the textbook for in Chapter 11)
As in previous assignments, you will need to research a variety of additional information such as required formulas and pertinent aircraft data and/or assume a few parameters for your aircraft. Please make sure to detail those:
Required Formulas:
Bank angle to G relationship
Turn rate and radius
Stall speed under elevated G / bank
Necessary aircraft information:
Limiting load factors (positive and negative) for your example aircraft (from research)
Assumed aircraft weight
Previous information:
Utilize your previous module work to find 1G stall speed for your selected weight
Assume atmospheric conditions
Again, the emphasis in this project task is on explaining your methodology as if you attempted to instruct someone unfamiliar with the aerodynamic details and relationships. Therefore, make sure to detail all assumptions, all formulas used, and all steps that were taken.
As previously stated, you are encouraged to utilize appropriate computational software such as Excel® Links to an external site.or MATLAB®. Links to an external site. (Linked, are the ERAU guides to access this software.)

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