Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missile Configuration at Mach 1.50 to 2.86 PDF Download

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Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missile Configuration at Mach 1.50 to 2.86

Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missile Configuration at Mach 1.50 to 2.86 PDF Author: Lloyd S. Jernell
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missile Configuration at Mach 1.50 to 2.86

Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missile Configuration at Mach 1.50 to 2.86 PDF Author: Lloyd S. Jernell
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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Book Description

Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missle Configuration at Mach 1.550 to 2.86

Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missle Configuration at Mach 1.550 to 2.86 PDF Author: Lloyd S. Jernell
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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Book Description

Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.16 of a Blunt-nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins

Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.16 of a Blunt-nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins PDF Author: William J. Monta
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36

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Effects of Nose Bluntness on the Static Aerodynamic Characteristics of a Cruciform Wing Missile at Mach Numbers 1.50 to 2.86

Effects of Nose Bluntness on the Static Aerodynamic Characteristics of a Cruciform Wing Missile at Mach Numbers 1.50 to 2.86 PDF Author: Roger H. Fournier
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

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Book Description

Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Model Base on the Static Aerodynamic Characteristics of Blunt Bodies at Mach Numbers of 1.57, 1.80, and 2.16 and Angles of Attack Up to 180 ̊

Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Model Base on the Static Aerodynamic Characteristics of Blunt Bodies at Mach Numbers of 1.57, 1.80, and 2.16 and Angles of Attack Up to 180 ̊ PDF Author: David S. Shaw
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 88

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Preliminary Investigation of the Effects of Several Seeker-nose Configurations on the Longitudinal Characteristics of a Canard-type Missile at a Mach Number of 1.60

Preliminary Investigation of the Effects of Several Seeker-nose Configurations on the Longitudinal Characteristics of a Canard-type Missile at a Mach Number of 1.60 PDF Author: A. Warner Robins
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 32

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Book Description

Effect of Nose Bluntness and Afterbody Shape on Aerodynamic Characteristics of a Monoplanar Missile Concept with Bodies of Circular and Elliptical Cross Sections at a Mach Number of 2.50

Effect of Nose Bluntness and Afterbody Shape on Aerodynamic Characteristics of a Monoplanar Missile Concept with Bodies of Circular and Elliptical Cross Sections at a Mach Number of 2.50 PDF Author: Ernald B. Graves
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 100

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Longitudinal Stability and Control Characteristics of a Winged and a Flared Hypersonic Missile Configuration with Various Nose Shapes and Flare Modifications at a Mach Number of 2.01

Longitudinal Stability and Control Characteristics of a Winged and a Flared Hypersonic Missile Configuration with Various Nose Shapes and Flare Modifications at a Mach Number of 2.01 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

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Book Description

A Parametric Study of the Aerodynamic Characteristics of Nose-cylinder-flare Bodies at a Mach Number of 6.0

A Parametric Study of the Aerodynamic Characteristics of Nose-cylinder-flare Bodies at a Mach Number of 6.0 PDF Author: George C. Ashby
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 82

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Book Description

Longitudinal Stability and Control Characteristics of Missile Configurations Having Several Highly Swept Cruciform Fins and Number of Trailing Edge and Fin Tip Controls at Mach Nubmers from 2.21 to 6.01

Longitudinal Stability and Control Characteristics of Missile Configurations Having Several Highly Swept Cruciform Fins and Number of Trailing Edge and Fin Tip Controls at Mach Nubmers from 2.21 to 6.01 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 130

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Book Description