LO-120S is a german ultralight kit plane. More about it in the next link.
Jan 30, 2009
Jan 29, 2009
Lift Formula L = cV^2
Lift is proportional to some constants and the square of speed. Yes... square.
So if you are travelling faster your wing can be very small and vice versa.
And the factor of the speed is the most meaningfull in that formula since it is squared. Other factors have clearly less importance. So one should first fix the speeds for cruising and landing since that will affect the whole planning of the plane.
http://www.youtube.com/watch?v=zyfYeaSQbiA
http://www.youtube.com/watch?v=jz-b05dQ430&NR=1
So if you are travelling faster your wing can be very small and vice versa.
And the factor of the speed is the most meaningfull in that formula since it is squared. Other factors have clearly less importance. So one should first fix the speeds for cruising and landing since that will affect the whole planning of the plane.
http://www.youtube.com/watch?v=zyfYeaSQbiA
http://www.youtube.com/watch?v=jz-b05dQ430&NR=1
Jan 27, 2009
Airplane Valhalla in Mojave California
Jan 25, 2009
Innovative Airfoil Designs
Designers in Israel have invented (actually again) to fly always with flaps extracted. See the airfoil above.
The whole text is in AIAA-2003-603:
http://www.smart-uav.re.kr/lib/download_info.asp?path=file&filename=proceedings03.pdf
Check that for UAV wings also.
Aircraft Flutter Prevention
Check this YouTube video to find out how flutter occurs.
The following general principles are suggested to be observed for flutter prevention on ALL airplanes in the design of control surfaces and control systems.
1. Structural stiffness.
2. Elimination of all play in hinges and control-system joints.
3. Rigid interconnection between elevators.
4. A relatively low amount of aerodynamic balance!
5. High frictional damping (see ***1).
6. Adequate wing fillets and fairing.
7. Sharp leading edges on movable surfaces should be avoided.
*** 1. One idea might be to use gas springs at the control surfaces to get more damping and friction . See picture below.
Jan 21, 2009
Orion Cockpit Mock-up
Orion project engineer Jeff Fox shows some details of the design
YouTube video: "A Look Inside Orion"
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Labels:
Manned Space Flight,
Mock-ups,
Orion Spacecraft
Jan 20, 2009
Who was actually the first?
More about Karl Jatho:
http://www.karl-jatho.com/html/we_were_the_first.html
It is also possible that Gustave Whitehead was the first on.
http://www.flyingmachines.org/gwhtd.html
Here are some pictures of Karl Jatho's project.
http://www.karl-jatho.com/html/we_were_the_first.html
It is also possible that Gustave Whitehead was the first on.
http://www.flyingmachines.org/gwhtd.html
Here are some pictures of Karl Jatho's project.
Workshop.
Karl Jatho
Jan 19, 2009
Air Berlin Obtains Cat III-B Approval
"Air Berlin said it will be the first airline in Europe to carry out Category III-B instrument approaches with its Boeing 737NGs. The airline obtained approval for its fleet of 40 Boeing aircraft from Germany’s Federal Office of Civil Aviation (LBA). With Cat III-B authorization, the airline will be able to conduct landings with visibility down to 75 meters, reducing diversions to other airports. "
http://www.youtube.com/watch?v=rfFyZbO2dcc
http://en.wikipedia.org/wiki/Instrument_landing_system
http://www.youtube.com/watch?v=rfFyZbO2dcc
http://en.wikipedia.org/wiki/Instrument_landing_system
Super NLF Airfoil with Vortex Generators
Or extended run NLF airfoil.
Net drag reduction of 8 % (?) could be achieved. NLF airfoil was redesigned to have a longer laminar section and the aft flow was recovered by using small vortex generators at 75% or 85% chord position.
Some explaining pictures follow. The full text is in AIAA-2003-0211 "Enhanced Airfoil Design Incorporating Boundary Layer Mixing Devices".
Y-axis is the section lif coefficient cl and X-axis is the drag coefficient cd.
Net drag reduction of 8 % (?) could be achieved. NLF airfoil was redesigned to have a longer laminar section and the aft flow was recovered by using small vortex generators at 75% or 85% chord position.
Some explaining pictures follow. The full text is in AIAA-2003-0211 "Enhanced Airfoil Design Incorporating Boundary Layer Mixing Devices".
Y-axis is the section lif coefficient cl and X-axis is the drag coefficient cd.
Jan 18, 2009
Vortex Generators
Strange small devices found in many places. Do they really give you 5 % fuel saving and / or reduction of drag?
http://www.youtube.com/watch?v=f80a9jssUFU
http://en.wikipedia.org/wiki/Vortex_generator
http://www.microaero.com/
http://www.buyairtab.com/
http://www.fuelsavers.com.au/
The following video is telling no fuel savings (or too small).
http://www.youtube.com/watch?v=We8LWkqjdX4
The following source is telling other benefits.
http://www.youtube.com/watch?v=L508itf3oy8
http://www.youtube.com/watch?v=f80a9jssUFU
http://en.wikipedia.org/wiki/Vortex_generator
http://www.microaero.com/
http://www.buyairtab.com/
http://www.fuelsavers.com.au/
The following video is telling no fuel savings (or too small).
http://www.youtube.com/watch?v=We8LWkqjdX4
The following source is telling other benefits.
http://www.youtube.com/watch?v=L508itf3oy8
Jan 14, 2009
Acabion GTBO - Very Fast Motorbike
Jan 13, 2009
R.T. Youngman Full Span Flaps
Robert Talbot Youngman invented and patented full span flaps for small low wing airplane year 1946. Later these flaps were used in a test plane called Youngman-Baynes HL.1.
The innovative high-lift wing designed by R T Youngman was wedded to a re-designed Proctor Mk IV fuselage to evaluate fullspan slotted flaps. As VT789 the type was designated P.46 and flew on 5 February 1948 conferring excellent low speed lift. It was evaluated By RAE and later sold to the designer as G-AMBL.
General characteristics
Crew: 2
Length: 29 ft 0 in ()
Wingspan: 33 ft 0 in ()
Height: ()
Empty weight: 2,380 lb ()
Loaded weight: 3,500 lb ()
Powerplant: 1× de Havilland Gipsy Queen 25 6-cylinder inline, 250 hp ()
Performance
Maximum speed: 180 mph
The innovative high-lift wing designed by R T Youngman was wedded to a re-designed Proctor Mk IV fuselage to evaluate fullspan slotted flaps. As VT789 the type was designated P.46 and flew on 5 February 1948 conferring excellent low speed lift. It was evaluated By RAE and later sold to the designer as G-AMBL.
General characteristics
Crew: 2
Length: 29 ft 0 in ()
Wingspan: 33 ft 0 in ()
Height: ()
Empty weight: 2,380 lb ()
Loaded weight: 3,500 lb ()
Powerplant: 1× de Havilland Gipsy Queen 25 6-cylinder inline, 250 hp ()
Performance
Maximum speed: 180 mph
Jan 11, 2009
Caproni Ca 161 - Altitude Record Aircraft
CAPRONI Ca 161 bis was a world altitude record aircraft in piston powered propeller category.
As of 2007, this record still stands for piston-powered aircraft. On 8 May 1937, Lieutenant Colonel Mario Pezzi broke the world altitude record with a flight to 15,655 metres (51,362 ft). The following year, Pezzi broke the record again in the more powerful Ca.161bis, making a flight to 17,083 metres (56,032 ft) on 22 October 1938.
Specifications (Ca.161bis)
General characteristics
Crew: One pilot
Length: 8.25 m (27 ft 1 in)
Wingspan: 14.25 m (26 ft 9 in)
Height: 3.50 m (11 ft 6 in)
Wing area: 35.5 m² (382 ft²)
Empty weight: 1,205 kg (2,657 lb)
Gross weight: 1,650 kg (3,638 lb)
Powerplant: 1 × Piaggio P.XI R.C.100/2v, 560 kW (750 hp)
http://www.youtube.com/watch?v=AM4fCz6HjqM
Special pressurized suits were used during attempts, forefathers of modern space suits.
As of 2007, this record still stands for piston-powered aircraft. On 8 May 1937, Lieutenant Colonel Mario Pezzi broke the world altitude record with a flight to 15,655 metres (51,362 ft). The following year, Pezzi broke the record again in the more powerful Ca.161bis, making a flight to 17,083 metres (56,032 ft) on 22 October 1938.
Specifications (Ca.161bis)
General characteristics
Crew: One pilot
Length: 8.25 m (27 ft 1 in)
Wingspan: 14.25 m (26 ft 9 in)
Height: 3.50 m (11 ft 6 in)
Wing area: 35.5 m² (382 ft²)
Empty weight: 1,205 kg (2,657 lb)
Gross weight: 1,650 kg (3,638 lb)
Powerplant: 1 × Piaggio P.XI R.C.100/2v, 560 kW (750 hp)
http://www.youtube.com/watch?v=AM4fCz6HjqM
Special pressurized suits were used during attempts, forefathers of modern space suits.
* * *
Jan 10, 2009
Stearman-Hammond Y-1S - Trainer Airplane
Another interesting plane similar to Abrams Explorer is the Stearmann-Hammond Y-1S. The designs are almost identical and both were made just before the WW2. Y-1S is the smaller one.
http://www.youtube.com/watch?v=Jp3_vGRLewc
http://www.youtube.com/watch?v=Ve2SOo-3hUA&feature=related
1937
150hp Menasco C-4S;
span: 40'0"
length: 26'11"
load: 768#
v: 130/121/39
range: 480
Project was dropped in 1938. Maybe both planes were too strange and uckly for the pilots of that time?
http://www.youtube.com/watch?v=Jp3_vGRLewc
http://www.youtube.com/watch?v=Ve2SOo-3hUA&feature=related
1937
150hp Menasco C-4S;
span: 40'0"
length: 26'11"
load: 768#
v: 130/121/39
range: 480
Project was dropped in 1938. Maybe both planes were too strange and uckly for the pilots of that time?
Jan 6, 2009
Superpaper
Maybe soon full size planes will also be made of paper. Sweds have been able to make 7 times stronger paper.
http://www.livescience.com/technology/080705-nanopaper.html
http://www.livescience.com/technology/080705-nanopaper.html
~~~
Jan 1, 2009
Abrams Explorer - High Altitude Mapping Airplane
Picture shows the Abrams Explorer airplane. Here is a link to YouTube story about it:
http://www.youtube.com/watch?v=gsaAeLaNr60
And here is the Wikipedia page:
http://en.wikipedia.org/wiki/Abrams_P-1_Explorer
Year 1937 this plane must have been very special having nose gear, twin boom and pusher configuration. With small modifications this might be a nice "new design". The plane was also offered to Finnish Airforce 21.11.1938.
The plane is stored somewhere in USA waiting for restoration.
http://www.youtube.com/watch?v=gsaAeLaNr60
And here is the Wikipedia page:
http://en.wikipedia.org/wiki/Abrams_P-1_Explorer
Year 1937 this plane must have been very special having nose gear, twin boom and pusher configuration. With small modifications this might be a nice "new design". The plane was also offered to Finnish Airforce 21.11.1938.
The plane is stored somewhere in USA waiting for restoration.
Abrams Explorer 2007
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