Static Stability And Control Of Canard Configurations At Mach Numbers From 070 To 222 Trangular Wing And Canard With Twin Vertical Tails

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Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Trangular Wing and Canard with Twin Vertical Tails
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Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22
Language: en
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Type: BOOK - Published: 1961 - Publisher:

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The static aerodynamic characteristics of a canard airplane configuration having twin vertical stabilizing surfaces are presented. The model consisted of a wing
Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Longitudinal Characteristics of a Triangular Wing and Unswept Canard
Language: en
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The results of an investigation of the static longitudinal stability and control characteristics of a canard airplane configuration are presented without analys
Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Longitudinal Characteristics of an Unswept Wing and Canard
Language: en
Pages: 29
Authors: Victor L. Peterson
Categories: Airplanes
Type: BOOK - Published: 1958 - Publisher:

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The results of an investigation of the static longitudinal stability and control characteristics of a canard airplane configuration are presented without analys