Joined-wing and box-wing aircraft

hesham

ACCESS: USAP
Senior Member
Joined
26 May 2006
Messages
33,545
Reaction score
13,645
Hi,

a project for ring wing double deck airliner.
http://www.flightglobal.com/PDFArchive/View/2003/2003%20-%200326.html
 

Attachments

  • untitled.JPG
    untitled.JPG
    34.3 KB · Views: 942
Hi,

box-wing aircraft.
 

Attachments

  • box wing.jpg
    box wing.jpg
    2.9 KB · Views: 2,097
hesham,

where did you found that "box wing" airline. Could you please give us more details?

Thanks,

Antonio
 
hesham said:
Hi,

box-wing aircraft.

My dear Pometablava ,

I think the reference by my dear Boxkite contain the name of the site,that becuase
I don't remember its name now.
 
Hi,

http://www.abovetopsecret.com/forum/thread192824/pg1
 

Attachments

  • UAV 2.jpg
    UAV 2.jpg
    11.5 KB · Views: 158
  • UAV.jpg
    UAV.jpg
    17.1 KB · Views: 706
  • mt5q48.jpg
    mt5q48.jpg
    26.9 KB · Views: 1,210
  • mt5q1t.jpg
    mt5q1t.jpg
    26.1 KB · Views: 1,244
  • msc595.jpg
    msc595.jpg
    18.9 KB · Views: 1,329
  • msc23d.jpg
    msc23d.jpg
    19.6 KB · Views: 3,076
  • KA865.jpg
    KA865.jpg
    67.2 KB · Views: 1,293
Here's what I believed to be a CG concept drawing for a joined-wing glider. Picked this up from a foreign language forum which was using this to explain the joined-wing concept. There was no reference to this glider design perhaps members in know can assist.
 

Attachments

  • RD87E.jpg
    RD87E.jpg
    79.6 KB · Views: 261
Hi,

http://sysd.org/stas/taxonomy/term/9
 

Attachments

  • joined_wing.jpg
    joined_wing.jpg
    6.5 KB · Views: 2,819
  • ikelos.jpg
    ikelos.jpg
    11.4 KB · Views: 154
  • x-v8l.jpg
    x-v8l.jpg
    28.2 KB · Views: 117
A joined wing aircraft;
http://adg.stanford.edu/aa241/intro/futureac.html
 

Attachments

  • JWConcept.jpg
    JWConcept.jpg
    20.5 KB · Views: 134
Hi,

http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900005777_1990005777.pdf
 

Attachments

  • Rockwell.JPG
    Rockwell.JPG
    21.1 KB · Views: 121
  • joined wing.JPG
    joined wing.JPG
    24.3 KB · Views: 169
Hi,
Something more retro: The MAI-Kuzakov modified Po-2.

A scale model was wind-tested in 1951 by the Moscow Aviation Institute.

Photo and drawing from "Letatyelnyye Apparaty MAI" by Makarov, 1994
 

Attachments

  • Kuzakov Po-2.jpg
    Kuzakov Po-2.jpg
    52.9 KB · Views: 125
  • Kuzakov Po2.jpg
    Kuzakov Po2.jpg
    99.8 KB · Views: 128
This one was also designed and tested by the MAI, but I don't know the specifications and history.
Is there a 3V drawing available?
Photo from "Letatyelnyye Apparaty MAI" by Makarov, 1994
 

Attachments

  • MAI.jpg
    MAI.jpg
    346.4 KB · Views: 145
Thank you Retrofit;

it is very interesting projects,and anther joined wing aircraft
and high altitude surveillance aircarft.
http://aerade.cranfield.ac.uk/subject-listing/design.html
 

Attachments

  • 1.JPG
    1.JPG
    29 KB · Views: 163
  • 2.JPG
    2.JPG
    14.4 KB · Views: 172
Hi,

http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890009036_1989009036.pdf
 

Attachments

  • 1.JPG
    1.JPG
    24.1 KB · Views: 239
  • 2.JPG
    2.JPG
    24.9 KB · Views: 235
Also California Univ. joined-wing very large transport aircraft,it look
like Lockheed C-5 fuselage.

http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19940020238_1994020238.pdf
 

Attachments

  • 1.JPG
    1.JPG
    40.4 KB · Views: 374
Air Force Institute of Technology Report into "INERTIA MEASUREMENT AND DYNAMIC STABILITY ANALYSIS OF A RADIO-CONTROLLED JOINED-WING AIRCRAFT".

http: //www.dtic.mil/cgi-bin/GetTRDoc?AD=ADA451280&Location=U2&doc=GetTRDoc.pdf

"In 2004 and 2005 AFRL Air Vehicles Directorate designed, built, and flew a scaled radio-controlled joined-wing aircraft, called VA-1"
 
Hi,

From Lockheed Georgia,the Joined-wing long-endurance RPV.
http://www.flightglobal.com/pdfarchive/view/1987/1987%20-%200018.html
 

Attachments

  • RPV.JPG
    RPV.JPG
    29.4 KB · Views: 318
"UNIQUE STEALTH UNMANNED AERIAL VEHICLE - HOUCK AIRCRAFT DESIGN PROGRAM"
(A patented MAV/UAV joined-wing aerofoil concept)

(Volume 1: Program Overview)
http://www.dtic.mil/cgi-bin/GetTRDoc?AD=ADA494088&Location=U2&doc=GetTRDoc.pdf

(Volume 2: Prototype Report)
http://www.dtic.mil/cgi-bin/GetTRDoc?AD=ADA494062&Location=U2&doc=GetTRDoc.pdf

With funding....:

http://www.globalsecurity.org/military/library/budget/fy2006/usaf-peds/0602201F.pdf
http://www.globalsecurity.org/military/library/budget/fy2007/usaf-peds/0602201f.pdf
http://www.dtic.mil/descriptivesum/Y2008/AirForce/0602201F.pdf
 

Attachments

  • Houck.JPG
    Houck.JPG
    25.6 KB · Views: 310
Hi,

The Lockheed boxwing concept,please note;there is
no tail fin.
 

Attachments

  • boxwing.JPG
    boxwing.JPG
    20.9 KB · Views: 299
Retrofit said:
This one was also designed and tested by the MAI, but I don't know the specifications and history.
Is there a 3V drawing available?
Photo from "Letatyelnyye Apparaty MAI" by Makarov, 1994

1976 V. Kuznetsov drafted sport aerobatic aircraft "Photon-01" diamond-shaped wing. The aircraft is now intended to establish a piston engine M-337 260 hp with a tractor propeller.
 
John Wolkowitch's ACA Industries JW-1 and derivative projects:

index.php
 

Attachments

  • joinedwing1.jpg
    joinedwing1.jpg
    11.1 KB · Views: 1,235
  • File0109.jpg
    File0109.jpg
    122.3 KB · Views: 147
  • File0108.jpg
    File0108.jpg
    200.2 KB · Views: 111
  • rc-model.jpg
    rc-model.jpg
    82.9 KB · Views: 718
  • pop-sci-8601d.jpg
    pop-sci-8601d.jpg
    171.7 KB · Views: 762
  • pop-sci-8601c.jpg
    pop-sci-8601c.jpg
    110.5 KB · Views: 813
  • pop-sci-8601b.jpg
    pop-sci-8601b.jpg
    125.8 KB · Views: 822
  • pop-sci-8601a.png
    pop-sci-8601a.png
    108 KB · Views: 994
In 1977, Mr. Kuznetsov was designed to Moscow Aviation Institute super-heavy transport aircraft with diamond-shaped wing.
 

Attachments

  • 00а58.jpg
    00а58.jpg
    9.9 KB · Views: 224
The Green Flight Challenge will be held September 25 – October 1, 2011 at the Charles M. Schulz Sonoma County Airport in California. Nine teams are registered to compete in the competition. Team Synergy is led by John W. McGinnis. They are located in Montana. Their aircraft is a clean sheet design, featuring laminar flow, wake-immersed propulsion, open thermodynamics, subsonic area ruling, composite construction, and five seats. Synergy is currently registered and has met the FAA inspection.

Seats: 6
Max. power: 142 kW
Span: 32.0 ft
Energy type: Bio-diesel


Sources:
- http://www.synergyaircraft.com/
- Synergy: A Practical Lightplane for the New Century
- Proyecto Synergy, Buscando La Máxima Eficiencia
- NASA Green Flight Challenge: Conceptual Design Approaches and Technologies to Enable 200 Passenger Miles per Gallon
- Synergy on Facebook (access to many other pics)
 

Attachments

  • synergy-top-view.jpg
    synergy-top-view.jpg
    125.4 KB · Views: 107
  • Synergy-overhead.jpg
    Synergy-overhead.jpg
    6.2 KB · Views: 93
  • Synergy_v30_concept_b.jpg
    Synergy_v30_concept_b.jpg
    534.7 KB · Views: 95
  • synergy1.jpg
    synergy1.jpg
    27.4 KB · Views: 101
  • synergy.jpg
    synergy.jpg
    16.4 KB · Views: 106
Phew ! I had to go google the FW oddity.Despite looking like a turbo-prop, it is piston-engined, via an extension shaft...
 
Box wing or not, the wing surface is so ridiculous that I can't see that thing staying up in the air for a minute...
 
It doesn't look like there's enough wing area to produce sufficient lift to get that thing off of the ground. Though a simple solution would of course just be to increase the takeoff speed. ;D
 
Hi;


the Final optimized joined-wing aircraft configuration.
 

Attachments

  • Joined-wing.jpg
    Joined-wing.jpg
    58.2 KB · Views: 436
Can anyone summarise the advantages of these wings. Being joined do they have greater structural strength. The all seem much thinner then conventional wings - would that mean less room for fuel storage? Regards
 
In short: you have two wings of higher aspect ratio, and short chord. That might help some with achieving laminar flow (although the required sweep does not!).
The biggest plus is the fact that the wings are braced, so for a given strength they can be made lighter or with higher span. Both the high aspect ratio and the three-dimensional profile of the wing (seen from the front) help with induced drag.
 
Many thanks for the summary. Would such wings drive engines to be mounted of the main fuselage and not wing?
Regards
 
Zeppelin said:
Would such wings drive engines to be mounted of the main fuselage and not wing?
Regards
You'll note in the various pictures the power plants are mounted on the wings in some designs and not on others. If the design uses thinner, longer, high aspect ratio wings then the power plants are probably going to be on the fuselage for strength and power carry-through reasons. If the wings CAN hold the engines then they probably will be mounted there such as in the Kuznetsov design shown. It's a design decision in the end.

BTW; I recall at one point seeing a drawing or "design" sketch of a BD-5J with joined/diamond wings and one point in time. Anyone else happen to recall seeing that or any information there-on?

Thanks

Randy
 
What is this aircraft ?.
 

Attachments

  • 1.jpg
    1.jpg
    38.4 KB · Views: 565
  • 2.jpg
    2.jpg
    91 KB · Views: 539
  • 3.jpg
    3.jpg
    61.8 KB · Views: 527

Similar threads

Please donate to support the forum.

Back
Top Bottom