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Results of search for 'au:"Giulianetti, Demo J"'

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Authors
- Giulianetti, Demo J (1)
- Giulianetti,Demo J (2)
- Maki,Ralph L (1)
- Weiberg,James A (1)
- Weilberg, James A (1)
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Holding libraries
- PK Kelkar Library, IIT Kanpur (4)
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- PK Kelkar Library, IIT Kanpur (4)
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- Technical Report (4)
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- National Aeronautics and Space Administration (NASA) (1)
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- Wind-tunnel (1)

Your search returned 4 results.

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	1.	LARGE-SCALE WIND TUNNEL TESTS OF ANAIRPLANE MODEL WITH AN UNSWEPT TILT WING OF ASPEECT RATIO 5.5, AND WITH VARIOUS STALL CONTROL DEVICES by Weiberg,James A \| Giulianetti,Demo J. Material type: Book Description: 42.Publisher: Nasa, Washington, D.C. 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D_2133 -] (1). Add to cart (remove)
	2.	WIND TUNNEL TEST OF A FULL-SCALE, 1.1 PRESSURE RATIO, DUCTED LIFT-CRUISE FAN by Giulianetti,Demo J, Biggers,James C \| Corsiglia,Victor R. Material type: Book Description: 45.Publisher: Nasa, Washington, D.C. 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2498 -] (1). Add to cart (remove)
	3.	Wind-tunnel investigation of a tilt-wing vtol-airplane with articulated rotors. [NASA TN D-2538] by Weilberg, James A \| Giulianetti, Demo J. Material type: Book; Format: print ; Literary form: not fiction Description: 55p.Publisher: Washington, D.C. Nasa 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2538] (1). Add to cart (remove)
	4.	LOW SPEED AERODYNAMIC CHARACTERISTICS OF A LARGE-SCALE MODEL WITH A THIN, HIGHLY SWEPT, 2.67 ASPECT RATIO WING HAVING A CRANKED LEADING EDGE by Giulianetti,Demo J \| Maki,Ralph L. Material type: Book Description: 39.Publisher: Nasa, Washington, D.C. 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-6919] (1). Add to cart (remove)

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