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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 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).

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 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).

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 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).

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 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).

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