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6 A is flight level when?

 
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mjurotich(at)hst.nasa.gov
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PostPosted: Wed Apr 19, 2006 6:23 am    Post subject: 6 A is flight level when? Reply with quote

I am near to getting my RV 6A back in the air after a complete
electrical and panel rebuild. I plan on redoing weight and
balance. With a slider is the top rail of the slider parallel to the
top longeron? The top longeron is Van's reference for on the ground
level. I presume the top longeron is "level" when in straight and
level flight.

Thanks

Matthew M. Jurotich

e-mail mail to: <mjurotich(at)hst.nasa.gov>
phone : 301-286-5919


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sportav8r(at)aol.com
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PostPosted: Wed Apr 19, 2006 9:52 am    Post subject: 6 A is flight level when? Reply with quote

That's (presumed to be) correct. Someday, I want to see numbers where someone has done their w&b with wheels level and with top longeron level, to see if the difference is truly worth worrying about. It's a lot of work to jack these planes into that configuration and chock the wheels and scales to correct heights (or dig a hole under the nosewheel Wink. I may do it myself if I get bored...

-Stormy

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khorton01(at)rogers.com
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PostPosted: Wed Apr 19, 2006 1:55 pm    Post subject: 6 A is flight level when? Reply with quote

On 19 Apr 2006, at 10:19, Matt Jurotich wrote:

Quote:


I presume the top longeron is "level" when in straight and
level flight.

The pitch attitude in straight and level flight will depend on the
airspeed, weight and flap angle, and to a less extent, on CG.

Kevin Horton RV-8 (finishing kit)
Ottawa, Canada
http://www.kilohotel.com/rv8


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lors01(at)msn.com
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PostPosted: Wed Apr 19, 2006 3:58 pm    Post subject: 6 A is flight level when? Reply with quote

True, which brings up a related subject.

Anyone know what the AOA of the 230xx airfoil on the RV is at any typical cruise speed? I need to make a decision on whether to change from stock RV incidence on my "long wing" RV-8. Span is 3 feet longer than stock which should result in a lower AOA for any given condition. I have a program to predict the appropriate change but don't know what it is to start with and haven't seen it in the plans book.

Tracy Crook
Quote:


I presume the top longeron is "level" when in straight and
level flight.

The pitch attitude in straight and level flight will depend on the
airspeed, weight and flap angle, and to a less extent, on CG.

Kevin Horton RV-8 (finishing kit)
Ottawa, Canada
http://www.kilohotel.com/rv8<http://www.kilohotel.com/rv8>


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klwerner(at)comcast.net
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PostPosted: Wed Apr 19, 2006 4:57 pm    Post subject: 6 A is flight level when? Reply with quote

Hi Tracy,
How come you extended your std. RV-8 Wings to become 3ft. longer?
Just curious to find out your reason.

Do not archive

SNIP
..on my "long wing" RV-8. Span is 3 feet longer than stock ...
SNIP

Tracy Crook


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khorton01(at)rogers.com
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PostPosted: Wed Apr 19, 2006 5:25 pm    Post subject: 6 A is flight level when? Reply with quote

The AOA will be quite low. If the airfoil was a true 23013.5 series,
and this was a 2D wing (i.e. there were no effects from the fuselage
or wing tip, the AOA at 1600 lb, 212 mph at 8,000 ft would be about
0.3 degrees (value calculated by XFOIL). If we drop the cruise speed
to 189 mph, the AOA would be about 0.6 degrees.

I understand that the leading edge of the RV airfoil differs slightly
from the NACA profile. And, the local AOA is not constant along the
span, due to the effect of the fuselage and wing tip. So the above
values must be considered as approximate.

Kevin Horton

On 19 Apr 2006, at 19:55, Tracy Crook wrote:

Quote:


True, which brings up a related subject.

Anyone know what the AOA of the 230xx airfoil on the RV is at any
typical cruise speed? I need to make a decision on whether to
change from stock RV incidence on my "long wing" RV-8. Span is 3
feet longer than stock which should result in a lower AOA for any
given condition. I have a program to predict the appropriate
change but don't know what it is to start with and haven't seen it
in the plans book.

Tracy Crook
>
> <mjurotich(at)hst.nasa.gov<mailto:mjurotich(at)hst.nasa.gov>>
>
> I presume the top longeron is "level" when in straight and
> level flight.

The pitch attitude in straight and level flight will depend on the
airspeed, weight and flap angle, and to a less extent, on CG.

Kevin Horton RV-8 (finishing kit)
Ottawa, Canada
http://www.kilohotel.com/rv8<http://www.kilohotel.com/rv8>


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low pass



Joined: 10 Jan 2006
Posts: 32
Location: Houston

PostPosted: Wed Apr 19, 2006 6:03 pm    Post subject: Re: 6 A is flight level when? Reply with quote

Tracy -

Regarding the 3' longer wings, did you consider the change in flutter characteristics of the new wings? How about longitudinal stability?

Not trying to be a downer on new ideas, but I would be very concerned about the change in resonance characteristics of the wing. And to a lesser degree the stability.

Just curious

Bryan Jones, PE, -8
Houston, Texas


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randy(at)romeolima.com
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PostPosted: Wed Apr 19, 2006 8:15 pm    Post subject: 6 A is flight level when? Reply with quote

The standard angle of incidence on the RV-4 and RV-8 is .5 degrees. The
guppy planes (side-by-side) are 1.0 degrees. Curiously the RV-3 is also 1.0
degrees.

Randy Lervold

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