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1. AN EXPERIMENTAL INVESTIGATION OF THE EFFECT OF A CANARD CONTROL ON THE LIFT, DRAG, AND PITCHING MOMENT OF AN ASPECT-RATIO-2.O TRIANGULAR WING INCORPORATING A FORM OF CONICAL CAMBER

by Menees,Gene P | Boyd,John W.

Material type: book Book Description: 29.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA MEMO 5-20-59A] (1).

2. NASA Memorandum [NASA MEMO 4-21-59A]: Longitudinal stability and control characteristics at mach numbers from 0.70 to 2.22 of a triangular wing configuration equipped with a canard control, a trailing-edge-flap control or a cambered forebody

by Washington. National Aeronautics and Space Administration (NASA) | Boyd, John W | Menees, Gene P.

Material type: book Book Description: 39p.Publisher: Washington NASA 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

3. An experimental investigation of a triangular wing of aspect ration 2 and a body warped to be trimmed at M=224 [Gaynor J. Adoms and John W. Boyd]

by Adams, Gaynor J | Boyd, John W.

Material type: book Book; Format: print ; Literary form: not fiction Description: 38p.Publisher: Washington National Aeronautics and Space Administration 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

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