Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.4 to 2.3 of a Rocket-powered Model Having a 52.5 Degree Sweptback Wing of Aspect Ratio 3 and Inline Tail Surfaces PDF Download

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Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.4 to 2.3 of a Rocket-powered Model Having a 52.5 Degree Sweptback Wing of Aspect Ratio 3 and Inline Tail Surfaces

Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.4 to 2.3 of a Rocket-powered Model Having a 52.5 Degree Sweptback Wing of Aspect Ratio 3 and Inline Tail Surfaces PDF Author: Warren Jr Gillespie
Publisher:
ISBN:
Category :
Languages : en
Pages : 29

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Book Description

Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.4 to 2.3 of a Rocket-powered Model Having a 52.5 Degree Sweptback Wing of Aspect Ratio 3 and Inline Tail Surfaces

Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.4 to 2.3 of a Rocket-powered Model Having a 52.5 Degree Sweptback Wing of Aspect Ratio 3 and Inline Tail Surfaces PDF Author: Warren Jr Gillespie
Publisher:
ISBN:
Category :
Languages : en
Pages : 29

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Book Description

Lift, Drag, and Longitudinal Stability at Mach Numbers from 0.8 to 2.1 of a Rocket-powered Model Having a Tapered Unswept Wing of Aspect Ratio 3 and Inline Tail Surfaces

Lift, Drag, and Longitudinal Stability at Mach Numbers from 0.8 to 2.1 of a Rocket-powered Model Having a Tapered Unswept Wing of Aspect Ratio 3 and Inline Tail Surfaces PDF Author: Warren Jr Gillespie
Publisher:
ISBN:
Category :
Languages : en
Pages : 29

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Longitudinal Stability and Drag Characteristics at Mach Numbers from 0.70 to 1.37 of Rocket-propelled Models Having a Modified Triangular Wing

Longitudinal Stability and Drag Characteristics at Mach Numbers from 0.70 to 1.37 of Rocket-propelled Models Having a Modified Triangular Wing PDF Author: Rowe Jr Chapman
Publisher:
ISBN:
Category :
Languages : en
Pages : 35

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Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing

Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing PDF Author: Edward J. Ray
Publisher:
ISBN:
Category :
Languages : en
Pages : 84

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Drag Due to Lift at Mach Numbers Up to 2.0

Drag Due to Lift at Mach Numbers Up to 2.0 PDF Author: Edward C. Polhamus
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 28

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Rocket-powered Model Investigation of Lift, Drag, and Stability of a Body-tail Configuration at Mach Numbers from 0.8 to 2.3 and Angles of Attack Between Plus Or Minus 6.5 Degrees

Rocket-powered Model Investigation of Lift, Drag, and Stability of a Body-tail Configuration at Mach Numbers from 0.8 to 2.3 and Angles of Attack Between Plus Or Minus 6.5 Degrees PDF Author: Warren Jr Gillespie
Publisher:
ISBN:
Category :
Languages : en
Pages : 42

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Aerodynamic Characteristics at Mach Numbers from 0.50 to 2.96 of a Supersonic Transport Model with a Variable-sweep High-panel-aspect-ratio Wing

Aerodynamic Characteristics at Mach Numbers from 0.50 to 2.96 of a Supersonic Transport Model with a Variable-sweep High-panel-aspect-ratio Wing PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 94

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Lift and Drag Characteristics at Subsonic Speeds and at a Mach Number of 1.9 of a Lifting Circular Cylinder with a Fineness Ratio of 10

Lift and Drag Characteristics at Subsonic Speeds and at a Mach Number of 1.9 of a Lifting Circular Cylinder with a Fineness Ratio of 10 PDF Author: Vernard E. Lockwood
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 26

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Launch, Low-speed, and Landing Characteristics Determined from the First Flight of the North American X-15 Research Airplane

Launch, Low-speed, and Landing Characteristics Determined from the First Flight of the North American X-15 Research Airplane PDF Author: Thomas W. Finch
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 30

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Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82

Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82 PDF Author: Ross B. Robinson
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 38

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Book Description