UAV-ARDA mk 9 "XB-35"

Advanced Reduced Drag Aircraft
By Jean-Louis Naudin
created on April 28, 2002 - JLN Labs - Last update April 30, 2002


" The flying wing airplane is the most evocative shape in aviation : a pure wing, unencumbered by tail surfaces or a fuselage, producing lift over every square meter of its surface. ". Richard P. Hallion (PhD), the US Air Force historian.

" L'aile volante représente la configuration aéronautique la plus aboutie : une aile dont la pureté n'est pas altérée par des empennages ou un fuselage, et dont chaque mètre carré de sa surface génère de la portance ". Richard P. Hallion (PhD), directeur du service historique de l'US Air Force.

Note from JL Naudin : This model is the 1/14 scale model of the Northrop XB-35 Flying Wing build by Jack Northrop in 1946. It is full powered by electric energy and able to fly up to 10 minutes.

See the VIDEO of the XB-35 test flight


Click on the picture to see the video ( 876 kb )


See also :

The Northrop Shock Wave Reduction experiment

The ARDA Mk 9, Test flight successful on March 24, 2002

ARDA mk8 "N9-M" - Flights Tests successful on August 25th, 2001


Additional notes :

For those are interested to know more about the air drag reduction researches conducted by Northrop, I suggest to read :

- AIAA 6th Aerospace Sciences Meeting " Electroaerodynamics in supersonic flow" by M.S.Cahn and G.M.Andrew from Northrop Coporation - N°68-24 January
22-24, 1968

- AIAA 3rd Fluid and Plasma Dynamics conference" Recent experiments in supersonic regime with electrostatic charges"  by M.S.Cahn and G.M.Andrew
from Northrop Coporation - N°70-759 June 29-July, 1970

You will find also some interesting informations about some projects on Hypersonic experiments at Mach numbers from 8 to 25 don by the RPI (
Reensselaer Polytechnic Institute ) at :
http://lightcraft.meche.rpi.edu/Facilities/hypersonic_shock_tunnel.html

- AIAA 98-0991 "Pressure Investigation of the Hypersonic "Directed-Energy Air Spike" Inlet at Mach Number 10 With Arc Power Up to 70 kW", Toro, P.G.P,
Myrabo, L.N., Nagamatsu, H.T., January, 1998.


Email : JNaudin509@aol.com


Return to the Advanced Propulsions Researches page