Static Stability Characteristics of Blunt Low-fineness-ratio Bodies of Revolution at a Mach Number of 24.5 in Helium PDF Download

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Static Stability Characteristics of Blunt Low-fineness-ratio Bodies of Revolution at a Mach Number of 24.5 in Helium

Static Stability Characteristics of Blunt Low-fineness-ratio Bodies of Revolution at a Mach Number of 24.5 in Helium PDF Author: Robert D. Witcofski
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 54

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Static Stability Characteristics of Blunt Low-fineness-ratio Bodies of Revolution at a Mach Number of 24.5 in Helium

Static Stability Characteristics of Blunt Low-fineness-ratio Bodies of Revolution at a Mach Number of 24.5 in Helium PDF Author: Robert D. Witcofski
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 54

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Book Description

Static Stability Characteristics of Blunt Low-finess-ratio Bodies of Revolution at a Mach Number of 24.5 in Helium

Static Stability Characteristics of Blunt Low-finess-ratio Bodies of Revolution at a Mach Number of 24.5 in Helium PDF Author: Robert D. Witcofski
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

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Some Measurements of the Dynamic and Static Stability of Two Blunt-nosed, Low-fineness- Ratio Bodies of Revolution in Free Flight at Mequal4

Some Measurements of the Dynamic and Static Stability of Two Blunt-nosed, Low-fineness- Ratio Bodies of Revolution in Free Flight at Mequal4 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Investigation of the Normal-force, Axial-force, and Pitching-moment Characteristics of Blunt Low-fineness-ratio Bodies of Revolution at a Mach Number of 3.55

Investigation of the Normal-force, Axial-force, and Pitching-moment Characteristics of Blunt Low-fineness-ratio Bodies of Revolution at a Mach Number of 3.55 PDF Author: Russell W. McDearmon
Publisher:
ISBN:
Category : Axial loads
Languages : en
Pages : 36

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 932

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Static Longitudinal Stability of a Blunt-nosed Cylinder with Flared Afterbody at a Mach Number of 19.2

Static Longitudinal Stability of a Blunt-nosed Cylinder with Flared Afterbody at a Mach Number of 19.2 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28

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Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 10.9 to 21.2 in Helium

Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 10.9 to 21.2 in Helium PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 96

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TRANSONIC STATIC AERODYNAMIC CHARACTERISTICS OF A BLUNT CONECYLINDER BODY WITH FLARED AFTERBODIES OF VARIOUS ANGLES AND BASE AREAS

TRANSONIC STATIC AERODYNAMIC CHARACTERISTICS OF A BLUNT CONECYLINDER BODY WITH FLARED AFTERBODIES OF VARIOUS ANGLES AND BASE AREAS PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 52

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Transonic Static and Dynamic Longitudinal Stability Characteristics of a Low-fineness- Ratio, Blunted-cylinder Reentry Body Having a Converging-cone Afterbody

Transonic Static and Dynamic Longitudinal Stability Characteristics of a Low-fineness- Ratio, Blunted-cylinder Reentry Body Having a Converging-cone Afterbody PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28

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Longitudinal Stability and Drag Characteristics of a Fin-stabilized Body of Revolution with a Fineness Ratio of 12 as Measured by the Free-fall Method

Longitudinal Stability and Drag Characteristics of a Fin-stabilized Body of Revolution with a Fineness Ratio of 12 as Measured by the Free-fall Method PDF Author: Max C. Kurbjun
Publisher:
ISBN:
Category :
Languages : en
Pages : 19

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