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Comparison of Tests on Air Propellers in Flight with Wind Tunnel Model Tests on Similar Forms (1926)
NASA Technical Reports Server (NTRS) · leaf 6
5 COMPARISON OF TESTS ON AIR PROPELLERS ^1 00 I Camber ratio: Pitch: 5' 8.6". Pitch ratio: 0.7. Aspect ratio: 6 Pitch: .V 8.6". Pitch ratio: 0.7. Aspect ratio: 7.5. ('amber Minimum + 20 per cent. Rotation: Right hand. ratio: Minimum + 20 per cent. Rotation: Right hand. Fig. 3.—Experimental… … Pitch: 5' 1.2". Pitch ratio: 0.6. Aspect ratio: 6. Camber ratio: Pitch: 6' 3.2". Pitch ratio: 0.8. Aspect ratio: 6. Camber ratio: Minimum + 20 per cent. Rotation: Right hand. Minimum + 20 per cent. Rotation: Right hand. Fig. 5.—Experimental propeller B' for VE-7 airplane Fig. 4.—Experimental…NASA Technical Reports Server (NTRS)
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