Related Books

Flight Measurements of Stability and Control Derivatives of the X-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 250
Language: en
Pages: 56

Flight Measurements of Stability and Control Derivatives of the X-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 250

Authors: Roxanah B. Yancey
Categories: Mach number
Type: BOOK - Published: 1964 - Publisher:

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Flight Measurements of Stability and Control Derivatives of the X-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 25 Degrees
Language: en
Pages: 47

Flight Measurements of Stability and Control Derivatives of the X-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 25 Degrees

Authors: Roxannah B. Yancey
Categories:
Type: BOOK - Published: 1964 - Publisher:

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Flight Measurements of Stability and Control Derivatives of the X-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 25°
Language: en
Pages: 47

Flight Measurements of Stability and Control Derivatives of the X-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 25°

Authors: Roxanah B. Yancey
Categories: Mach number
Type: BOOK - Published: 1964 - Publisher:

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Aerodynamic-derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4
Language: en
Pages: 72

Aerodynamic-derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4

Authors: Roxanah B. Yancey
Categories:
Type: BOOK - Published: 1962 - Publisher:

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Stability and Control Derivative Characteristics of the X-15 Airplane
Language: en
Pages: 36

Stability and Control Derivative Characteristics of the X-15 Airplane

Authors: Harold J. Walker
Categories:
Type: BOOK - Published: 1962 - Publisher:

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