Why is Projected Area constant when varying AoA?

  • Thread starter Thread starter MD LAT 1492
  • Start date Start date
  • Tags Tags
    Area Constant
Click For Summary
SUMMARY

The projected area of streamlined and bluff bodies remains constant as a reference area despite variations in angles of attack (AoA). This convention is established to prevent confusion in aerodynamic calculations, particularly when comparing drag and lift coefficients. As noted by Aljoscha Sander, maintaining a constant reference area allows for accurate comparisons across different AoAs without complicating the analysis. Sarat C. Praharaj emphasizes the importance of consistency in using a fixed reference area to avoid confusion in aerodynamic assessments.

PREREQUISITES
  • Understanding of aerodynamic principles, specifically drag and lift coefficients.
  • Familiarity with the concept of angles of attack (AoA) in fluid dynamics.
  • Knowledge of reference area conventions in aerodynamic calculations.
  • Basic skills in interpreting polar diagrams related to drag and lift.
NEXT STEPS
  • Research the impact of varying angles of attack on drag and lift coefficients in aerodynamic bodies.
  • Learn about the conventions for selecting reference areas in aerodynamic analysis.
  • Explore the use of polar diagrams for visualizing drag and lift coefficients across different AoAs.
  • Investigate the relationship between projected area and aerodynamic performance in various body shapes.
USEFUL FOR

Aerodynamic engineers, students studying fluid dynamics, and researchers focused on drag and lift optimization will benefit from this discussion.

MD LAT 1492
Messages
7
Reaction score
3
For a streamlined and bluff bodies, why is it standard to have the projected area be a fixed reference area, but yet the angles of attack (AoA) vary? If one were to vary the AoA then the projected area would technically change.

The following link discusses that it is a convention to avoid confusion. https://www.researchgate.net/post/What_should_be_the_reference_area_for_calculating_drag_and_lift_coefficients_in_case_of_elliptic_cylinder

My attempt included drawing it up and then projecting it with an arbitrary AoA.
But the projected areas never reduced down to the convention. I appreciate you talking the time to to provide any guidance! Thank you
 
Physics news on Phys.org
Hi @MD LAT 1492 , from reading the URL you shared, it appears that the confusion comes from this point: While the drag and coefficient of drag (Cd) of the body will vary with AoA, the Reference Area will not. The responses seem to indicate that you can either vary the projected area, or the drag coefficient, as you change your AoA.

Quoting Aljoscha Sander from the forum. you shared:

"However, If you want to compare angles of attack (for instance in a polar diagram with drag and lift coefficients) length scale and projected area should stay constant at all times."

On the other side of the same coin, for a given body, you could cite the change in projected area and length scale at each drag coefficient. This, would be incredibly confusing, and I believe that's what Sarat C. Praharaj was getting at when he mentioned:

"...any reference area is good so long as you are consistent. Don't vary that with angle of attack, because you will confuse yourself and others by doing that. Just use the major axis for the length scale."

I believe that hey are choosing to use a fixed area and length as reference, to find Cd/Cl at varying AoAs, by convention.

Cheers!
 
  • Like
Likes   Reactions: MD LAT 1492 and FactChecker

Similar threads

  • · Replies 20 ·
Replies
20
Views
3K
  • · Replies 6 ·
Replies
6
Views
16K
  • · Replies 5 ·
Replies
5
Views
9K
  • · Replies 35 ·
2
Replies
35
Views
11K
Replies
2
Views
665
Replies
3
Views
6K
  • · Replies 1 ·
Replies
1
Views
2K
Replies
2
Views
9K
  • · Replies 9 ·
Replies
9
Views
4K
  • · Replies 7 ·
Replies
7
Views
2K