Matches in DBpedia 2014 for { <http://dbpedia.org/resource/Akaflieg_Darmstadt_D-40> ?p ?o. }
Showing items 1 to 48 of
48
with 100 items per page.
- Akaflieg_Darmstadt_D-40 abstract "The Akaflieg Darmstadt D-40 is an experimental variable geometry single seat sailplane, fitted with almost full span, camber changing flaps for optimum aerodynamics in weak thermals and integrated into the wing so as to minimise flap tip drag. One flew successfully but the D-40, like other variable geometry sailplanes, was not commercialised.".
- Akaflieg_Darmstadt_D-40 manufacturer Akaflieg_Darmstadt.
- Akaflieg_Darmstadt_D-40 numberBuilt "1".
- Akaflieg_Darmstadt_D-40 origin Germany.
- Akaflieg_Darmstadt_D-40 type Experimental_aircraft.
- Akaflieg_Darmstadt_D-40 wikiPageExternalLink fx60126.gif.
- Akaflieg_Darmstadt_D-40 wikiPageExternalLink d-40.
- Akaflieg_Darmstadt_D-40 wikiPageID "34533093".
- Akaflieg_Darmstadt_D-40 wikiPageRevisionID "601424606".
- Akaflieg_Darmstadt_D-40 airfoil "Inner Wortmann 67 - VG - 170 ; at tips, Wortmann FX60 - 126".
- Akaflieg_Darmstadt_D-40 aspectRatio "23.7".
- Akaflieg_Darmstadt_D-40 crew "1".
- Akaflieg_Darmstadt_D-40 designer "K. J. Heer and D. Teves".
- Akaflieg_Darmstadt_D-40 emptyWeightKg "284".
- Akaflieg_Darmstadt_D-40 firstFlight "1986-08-15".
- Akaflieg_Darmstadt_D-40 gLimits "+5.3/-2.6".
- Akaflieg_Darmstadt_D-40 grossWeightKg "374".
- Akaflieg_Darmstadt_D-40 grossWeightNote "Maximum 500 kg with water ballast".
- Akaflieg_Darmstadt_D-40 hasPhotoCollection Akaflieg_Darmstadt_D-40.
- Akaflieg_Darmstadt_D-40 heightM "1.47".
- Akaflieg_Darmstadt_D-40 lengthM "6.75".
- Akaflieg_Darmstadt_D-40 manufacturer Akaflieg_Darmstadt.
- Akaflieg_Darmstadt_D-40 maxSpeedKmh "295".
- Akaflieg_Darmstadt_D-40 maxSpeedNote "smooth air; rough air and aero-tow 190 km/h".
- Akaflieg_Darmstadt_D-40 nationalOrigin Germany.
- Akaflieg_Darmstadt_D-40 numberBuilt "1".
- Akaflieg_Darmstadt_D-40 primeUnits%3F_ "met".
- Akaflieg_Darmstadt_D-40 ref "Jane's All the World's Aircraft 1987/8".
- Akaflieg_Darmstadt_D-40 spanM "15".
- Akaflieg_Darmstadt_D-40 stallSpeedKts "35".
- Akaflieg_Darmstadt_D-40 type "Experimental high performance sailplane".
- Akaflieg_Darmstadt_D-40 wingAreaNote "flap retracted; 11.5 m² extended".
- Akaflieg_Darmstadt_D-40 wingAreaSqm "9.5".
- Akaflieg_Darmstadt_D-40 m "34.74".
- Akaflieg_Darmstadt_D-40 wingLoadingNote "minimum, flaps in, 52.63 kg/m² maximum. Flaps out, 28.70 kg/m² minimum, 43.48 kg/m² maximum".
- Akaflieg_Darmstadt_D-40 subject Category:German_sailplanes_1980–1989.
- Akaflieg_Darmstadt_D-40 type Aircraft.
- Akaflieg_Darmstadt_D-40 type MeanOfTransportation.
- Akaflieg_Darmstadt_D-40 type Product.
- Akaflieg_Darmstadt_D-40 type DesignedArtifact.
- Akaflieg_Darmstadt_D-40 comment "The Akaflieg Darmstadt D-40 is an experimental variable geometry single seat sailplane, fitted with almost full span, camber changing flaps for optimum aerodynamics in weak thermals and integrated into the wing so as to minimise flap tip drag. One flew successfully but the D-40, like other variable geometry sailplanes, was not commercialised.".
- Akaflieg_Darmstadt_D-40 label "Akaflieg Darmstadt D-40".
- Akaflieg_Darmstadt_D-40 sameAs m.0j272yr.
- Akaflieg_Darmstadt_D-40 sameAs Q4700112.
- Akaflieg_Darmstadt_D-40 sameAs Q4700112.
- Akaflieg_Darmstadt_D-40 wasDerivedFrom Akaflieg_Darmstadt_D-40?oldid=601424606.
- Akaflieg_Darmstadt_D-40 homepage d-40.
- Akaflieg_Darmstadt_D-40 isPrimaryTopicOf Akaflieg_Darmstadt_D-40.