Effectiveness of Two Flap Controls on a Mercury Type Capsule at a Mach Number of 15 in the Ames Hypersonic Helium Tunnel PDF Download

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Effectiveness of Two Flap Controls on a Mercury Type Capsule at a Mach Number of 15 in the Ames Hypersonic Helium Tunnel

Effectiveness of Two Flap Controls on a Mercury Type Capsule at a Mach Number of 15 in the Ames Hypersonic Helium Tunnel PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28

Book Description

Effectiveness of Two Flap Controls on a Mercury Type Capsule at a Mach Number of 15 in the Ames Hypersonic Helium Tunnel

Effectiveness of Two Flap Controls on a Mercury Type Capsule at a Mach Number of 15 in the Ames Hypersonic Helium Tunnel PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28

Book Description

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 444

Book Description

Pressure and Heat-transfer Distribution on the Afterbody of a Lifting Mercury-type Capsule at Mach Number 15 in Helium

Pressure and Heat-transfer Distribution on the Afterbody of a Lifting Mercury-type Capsule at Mach Number 15 in Helium PDF Author: Joseph G. Marvin
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 40

Book Description

Effects of Angle of Attack and Bluntness on the Hypersonic Flow Over a 15 ̊semiapex Cone in Helium

Effects of Angle of Attack and Bluntness on the Hypersonic Flow Over a 15 ̊semiapex Cone in Helium PDF Author: Joseph W. Cleary
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 52

Book Description

Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium

Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium PDF Author: Melvin J. Fohrman
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48

Book Description

An Exploratory Investigation at a Mach Number of 6.9 Into the Use of Aerodynamic Controls for Modulating the Lift-drag Ratio of an Apollo Type Configuration

An Exploratory Investigation at a Mach Number of 6.9 Into the Use of Aerodynamic Controls for Modulating the Lift-drag Ratio of an Apollo Type Configuration PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28

Book Description

Experimental Investigation of the Flow Field and Heat Transfer Over the Apollo-capsule Afterbody at a Mach Number of 20

Experimental Investigation of the Flow Field and Heat Transfer Over the Apollo-capsule Afterbody at a Mach Number of 20 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

Book Description

Pressure and Heat-transfer Distribution on the Afterbody of a Lifting Mercury- Type Capsule at Mach Number 15 in Helium

Pressure and Heat-transfer Distribution on the Afterbody of a Lifting Mercury- Type Capsule at Mach Number 15 in Helium PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

Book Description

Theoretical and Experimental Longitudinal and Lateral Static Stability and Control Characteristics of a Series of Axisymmetric High Drag Reentry Vehicles at a Mach Number of 6.7

Theoretical and Experimental Longitudinal and Lateral Static Stability and Control Characteristics of a Series of Axisymmetric High Drag Reentry Vehicles at a Mach Number of 6.7 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 84

Book Description

Telemetry Measurements of Afterbody Pressures on Free-flying Models of the Apollo Capsule at Mach Numbers from 10 to 21 in Helium and 14 in Air

Telemetry Measurements of Afterbody Pressures on Free-flying Models of the Apollo Capsule at Mach Numbers from 10 to 21 in Helium and 14 in Air PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 42

Book Description

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