Aerodynamic Forces on 6' x 3' plate at 45 degrees - 70 MPH?

In summary, the diverter plane on the tow vehicle is likely not doing much good with the airflow over the trailer.
  • #1
kach22i
51
0
Thread for context this question came up in:
http://ecomodder.com/forum/showthre...l-economy-tonneau-cover-124-6.html#post535358
Untitled8_10.jpg


Does anyone have any idea of what kind of forces a 6 foot wide, 3 foot long wing would see angled up into the wind at say a 45 degree angle or more at say up to 70 mpH?

I'm guessing we will want the answer in pounds, perhaps FT/Pounds.

Ballpark numbers on horizontal, vertical and or down-force and or lift.

Just need a general idea for discussion purposes if you can please. Comparisons in laymen terms would be very useful.

My guess is that such a plane would experiences forces similar to a football tackle between some 120 lb kids. Not very useful, very subjective but it gets an image across hopefully.

Let's put it this way, if you have ever built something and sat on it, pulled on it, or jumped on it to test it before mounting, then you know what I mean. We are talking backyard engineering where one can just throw more parts and material on something until it feels right. Just short of the "hold my beer and watch this" approach.
 
Last edited:
Physics news on Phys.org
  • #2
Check out Hoerner's classic work on fluid dynamic drag and lift. Much of that was based on experimental work done in Germany in the 1930s, but it was good science.
 
  • #3
@kach22i -- That air dam on the SUV doesn't look like it's placed correctly. It sure doesn't seem to be doing much with the airflow over the trailer. Shouldn't it be placed at the back of the SUV, more in line with how the air dams on tractor-trailers work?

http://www.truck-drivers-money-saving-tips.com/image-files/air-resistance-drag-dsc09127.jpg
air-resistance-drag-dsc09127.jpg
 
  • Like
Likes Nidum
  • #4
Berkeman, I think they placed it correctly load wise, which is perhaps in conflict with aerodynamic needs.

In other words, the vertical force is downward and mid-way in the wheelbase of the tow vehicle.

If the vertical load is aft of the center of gravity it will lift the front wheels and steering gets light - way too light.

I've towed my hovercraft around a bit, once I tried loading it backwards with most of the weight on the tongue - that was a disaster in the making.

I think the rule of thumb with the sub 1,000 lb load I had was about 50 lbs on the tow hitch ball/tongue. I always like a little more weight because I was afraid of it lifting off the ball.

The double axle of the trailer/camper in the photo far above will still want to see-saw a bit, best to have your tow vehicle as sure footed as possible.
 
  • #5
Dr. D......back when I was in college 30 years ago I'm pretty sure I could have done this simple problem in 15 minutes.

I figured out earthquake and wind loads on multi-story buildings in my structural courses, I just didn't want to dust off my books and take the time.

This should be a simple problem for a smart person, I'm just not that smart anymore. I hire engineers to do my heavy lifting these days.
 
  • #6
kach22i said:
Berkeman, I think they placed it correctly load wise, which is perhaps in conflict with aerodynamic needs.

In other words, the vertical force is downward and mid-way in the wheelbase of the tow vehicle.

If the vertical load is aft of the center of gravity it will lift the front wheels and steering gets light - way too light.
Well, as it's placed right now, it looks like it is of no aerodynamic benefit to the trailer, and a significant aerodynamic hindrance to the SUV. I hope nobody pays any money for something like that.

To avoid the loading and downforce issues on the SUV, and help streamline the SUV+trailer pair, just run a taut tarp from the back of the SUV to the top/sides of the trailer. Make it so that it can flex for turning, but is taut enough to re-direct the airflow in straight-line high-speed driving so the front of the trailer is protected.
 
  • #7
I'm not here to argue the merits or efficiency of the design posted as I feel it's a distraction from the original goal stated.

I am more than willing to analyze it however in a effort to understand it.

I stated earlier that I thought the diverter plane was mid-point of the wheelbase or center of mass/gravity, this turns out not to be quite true (unlike the Tractor Trailer design). And as a result I'm starting to really not like it, although without a smoke flow image without the air diverter to compare to I'm hesitant to condemn it completely as of yet.

To make it clear, I'm not attempting to design or promote anything, just curious about the scale of forces involved.

It seems to me now that there could be more lot going on than I first thought, and this is not a simple vector of forces with equal reaction math problem. I mean it could be simple, not asking for axle loads or anything, right?

EDIT:
Untitled8_10.jpg

I found a sister image to the opening image - I think.

https://www.rv.net/forum/index.cfm/fuseaction/thread/tid/28963857/print/true.cfm
80-airflow_00207_f9d713c1ed92285e2dec0a3eba89274d9ae58277.jpg
 

Attachments

  • STUDY.jpg
    STUDY.jpg
    34.3 KB · Views: 542
Last edited:

1. What is the significance of studying aerodynamic forces on a 6' x 3' plate at 45 degrees and 70 MPH?

Studying aerodynamic forces on a plate at specific dimensions and angles can provide valuable insights into the effects of air resistance on objects moving at high speeds, such as vehicles or aircrafts. This information is crucial for optimizing aerodynamic designs and improving overall performance.

2. How are aerodynamic forces calculated on a 6' x 3' plate at 45 degrees and 70 MPH?

Aerodynamic forces are typically calculated using mathematical models and equations, such as the drag and lift equations. These equations take into account the dimensions, angle, and velocity of the plate, as well as other factors such as air density and viscosity.

3. What is the difference between drag and lift forces on a 6' x 3' plate at 45 degrees and 70 MPH?

Drag force is the resistance force acting in the opposite direction of motion, while lift force is the force perpendicular to the direction of motion. The drag force is primarily caused by air resistance, while the lift force is generated by the difference in air pressure on the top and bottom surfaces of the plate.

4. How does the angle of the plate affect aerodynamic forces at 70 MPH?

The angle of the plate plays a significant role in determining the magnitude and direction of aerodynamic forces. At 45 degrees, the plate is at a high angle of attack, resulting in increased drag and lift forces. Changing the angle can alter the balance of these forces and impact the overall performance of the plate.

5. What are some practical applications of studying aerodynamic forces on a 6' x 3' plate at 45 degrees and 70 MPH?

The study of aerodynamic forces on plates can have a wide range of practical applications, such as in the design and optimization of vehicles, aircrafts, and sports equipment. It can also be used in the development of wind turbines and other structures that are exposed to high wind speeds.

Similar threads

Replies
35
Views
7K
  • Calculus and Beyond Homework Help
Replies
3
Views
3K
  • Introductory Physics Homework Help
Replies
6
Views
2K
  • Introductory Physics Homework Help
Replies
4
Views
3K
  • Introductory Physics Homework Help
Replies
1
Views
2K
Replies
6
Views
6K
Replies
2
Views
6K
  • Aerospace Engineering
Replies
5
Views
7K
Replies
2
Views
3K
Back
Top