Static Longitudinal And Lateral Stability Data From An Exploratory Investigation At Mach Number 406 Of An Airplane Configuration Having A Wing Of Trapezoidal Plan Form

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Static Longitudinal and Lateral Stability Data from an Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form

Static Longitudinal and Lateral Stability Data from an Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form

Author	: Robert W. Dunning
Publisher	:
Total Pages	: 37
Release	: 1955
Genre	:
ISBN	:

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Static Longitudinal and Lateral Stability Data from an Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form

Language: en
Pages: 37

Static Longitudinal and Lateral Stability Data from an Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form

Authors: Robert W. Dunning

Categories:

Type: BOOK - Published: 1955 - Publisher:

Static Longitudinal and Lateral Stability and Control Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form

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Static Longitudinal and Lateral Stability and Control Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form

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Lift, Drag, and Static Longitudinal Stability Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form

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Pages: 34

Lift, Drag, and Static Longitudinal Stability Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form

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Categories: Airplanes

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Static Lateral Stability Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plam Form

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Static Lateral Stability Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plam Form

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Type: BOOK - Published: 1955 - Publisher:

Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane

Language: en
Pages: 150

Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane

Authors: Jim A. Penland

Categories: Aerodynamic measurements

Type: BOOK - Published: 1960 - Publisher: