Related Books

Effects of Wing Vertical Location 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
Language: en
Pages: 44

Effects of Wing Vertical Location 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

Authors: Gerald V. Foster
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1959 - Publisher:

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Effects of Wing Vertical Location on Stability and Control Characteristics at Mach Number of 2.01 of Canard Airplane Configuration with Trapezoidal Aspect-ratio-3 Wing [with List of References]
Language: en
Pages: 35

Effects of Wing Vertical Location on Stability and Control Characteristics at Mach Number of 2.01 of Canard Airplane Configuration with Trapezoidal Aspect-ratio-3 Wing [with List of References]

Authors:
Categories:
Type: BOOK - Published: 1959 - Publisher:

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Effects of Wing Height on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a 70° Delta Wing
Language: en
Pages: 42

Effects of Wing Height on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a 70° Delta Wing

Authors: Cornelius Driver
Categories: Airplanes
Type: BOOK - Published: 1960 - Publisher:

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The Effects of Wing Vertical Location and Vertical-tail Arrangement on the Stability Characteristics of Canard Airplane Configurations Having Delta and Trapezoidal Planforms at Mach Numbers from 2.38 to 4.00
Language: en
Pages: 106

The Effects of Wing Vertical Location and Vertical-tail Arrangement on the Stability Characteristics of Canard Airplane Configurations Having Delta and Trapezoidal Planforms at Mach Numbers from 2.38 to 4.00

Authors: Frank H. Jr Nichols
Categories:
Type: BOOK - Published: 1961 - Publisher:

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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
Language: en
Pages: 36

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

Authors: M. Leroy Spearman
Categories: Airplanes
Type: BOOK - Published: 1962 - Publisher:

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