PKK Library catalog › Results of search for 'au:"Driver, Cornelius"'

1.

EFFECTS OF FOREBODY DEFLECTION ON STABILITY AND CONTROL CHARACTERISTICS OF A CANARD AIRPLANE CONFIGURATION WITH A HIGH TRAPEZOIDAL WING AT A MACH NUMBER OF 2.01

by Spearman,M Leroy | Driver,Cornelius.

Material type: book

Book Description: 28.Publisher: Nasa, Washington, D.C. 1959Availability: No items available Damaged (1).

2.

STABILITY AND CONTRL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS

by Driver,Cornelius | Spearman,M Leroy.

Material type: book

Book Description: 27.Publisher: Nasa, Washington, D.C. 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TM X-441] (1).

3.

EFFECTS OF FOREBODY LENGTH ON THE STABILITY AND CONTROL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A CANARD AIRPLANE CONFIGURATION WITH A TRAPEZOIDAL ASPECT-RATIO-3 WING

by Spearman,M Leroy | Driver,Cornelius.

Material type: book

Book Description: 30.Publisher: Nasa, Washington, D.C. 1962Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1263] (1).

4.

NASA Memo [10-1-58L] : longitudinal and lateral stability and control characteristics of various combinations of the component parts of two canard airplane configurations at mach numbers of 1.41 and 2.01

by Driver, Cornelius.

Description: 104p.Publisher: Washington National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

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