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
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 100

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Aerodynamic Characteristics of a Monoplanar Missile Concept with Bodies of Circular and Elliptical Cross Sections

Aerodynamic Characteristics of a Monoplanar Missile Concept with Bodies of Circular and Elliptical Cross Sections PDF Author: Ernald B. Graves
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ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 194

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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
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ISBN:
Category : Aerodynamics
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
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Category :
Languages : en
Pages : 36

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An Improved Semiempirical Method for Calculating Aerodynamics of Missiles with Noncircular Bodies

An Improved Semiempirical Method for Calculating Aerodynamics of Missiles with Noncircular Bodies PDF Author: Frankie Gale Moore
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Category : Aerodynamics
Languages : en
Pages : 148

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The Effect of Nose Shape and Afterbody Length on the Normal Force and Neutral Point Location of Axisymmetric Bodies at Mach Numbers from 0.80 to 4.50

The Effect of Nose Shape and Afterbody Length on the Normal Force and Neutral Point Location of Axisymmetric Bodies at Mach Numbers from 0.80 to 4.50 PDF Author: Donald J. Spring
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ISBN:
Category :
Languages : en
Pages : 35

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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
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ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 82

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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
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ISBN:
Category :
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
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ISBN:
Category :
Languages : en
Pages : 30

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Aerodynamic Characteristics of 0.187-scale Model of a Target Missile at Mach 1.80 to 2.16

Aerodynamic Characteristics of 0.187-scale Model of a Target Missile at Mach 1.80 to 2.16 PDF Author: William A. Corlett
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ISBN:
Category :
Languages : en
Pages : 84

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