The Effect of Nose Shape and Afterbody Length on the Normal Force and Neutral Point Location of Axisymmetric Bodies at Mach Numers from 0.08 to 4.50 PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download The Effect of Nose Shape and Afterbody Length on the Normal Force and Neutral Point Location of Axisymmetric Bodies at Mach Numers from 0.08 to 4.50 PDF full book. Access full book title The Effect of Nose Shape and Afterbody Length on the Normal Force and Neutral Point Location of Axisymmetric Bodies at Mach Numers from 0.08 to 4.50 by Donald Jacob Spring. Download full books in PDF and EPUB format.

The Effect of Nose Shape and Afterbody Length on the Normal Force and Neutral Point Location of Axisymmetric Bodies at Mach Numers from 0.08 to 4.50

The Effect of Nose Shape and Afterbody Length on the Normal Force and Neutral Point Location of Axisymmetric Bodies at Mach Numers from 0.08 to 4.50 PDF Author: Donald Jacob Spring
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 92

Get Book Here

Book Description

The Effect of Nose Shape and Afterbody Length on the Normal Force and Neutral Point Location of Axisymmetric Bodies at Mach Numers from 0.08 to 4.50

The Effect of Nose Shape and Afterbody Length on the Normal Force and Neutral Point Location of Axisymmetric Bodies at Mach Numers from 0.08 to 4.50 PDF Author: Donald Jacob Spring
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 92

Get Book Here

Book Description

Summary of Static Stability and Drag Characteristics of Axisymmetric Low-drag Shapes for the Subsonic to Hypersonic Mach Number Range

Summary of Static Stability and Drag Characteristics of Axisymmetric Low-drag Shapes for the Subsonic to Hypersonic Mach Number Range PDF Author: Amado A. Trujillo
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 44

Get Book Here

Book Description

A Wind-tunnel Investigation of Effects of Noise Bluntness, Face Shape, and Afterbody Length on the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90

A Wind-tunnel Investigation of Effects of Noise Bluntness, Face Shape, and Afterbody Length on the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 48

Get Book Here

Book Description

Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85

Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85 PDF Author: Reino J. Salmi
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 22

Get Book Here

Book Description

A Wind-tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 at Angles of Attack to 90 Deg

A Wind-tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 at Angles of Attack to 90 Deg PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

Get Book Here

Book Description

Some Effects of Nose Bluntness and Fineness Ration on the Static Longitudinal Aerodynamic Characteristics of Bodies of Revolution at Bussonic Speeds

Some Effects of Nose Bluntness and Fineness Ration on the Static Longitudinal Aerodynamic Characteristics of Bodies of Revolution at Bussonic Speeds PDF Author: William C. Hayes
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 70

Get Book Here

Book Description

Effect of Cross-section Shape on the Aerodynamics Characteristics of Bodies at Mach Numbers from 2.50 to 4.63

Effect of Cross-section Shape on the Aerodynamics Characteristics of Bodies at Mach Numbers from 2.50 to 4.63 PDF Author: Dennis E. Fuller
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 40

Get Book Here

Book Description

Effects of Body Shape on the Aerodynamics of a Body of Revolution at Mach Numbers from 1.6 to 4.6

Effects of Body Shape on the Aerodynamics of a Body of Revolution at Mach Numbers from 1.6 to 4.6 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

Get Book Here

Book Description

Effect of Afterbody Geometry and Sting Diameter on the Aerodynamic Characteristics of Slender Bodies at Mach Number from 1.57 to 2.86

Effect of Afterbody Geometry and Sting Diameter on the Aerodynamic Characteristics of Slender Bodies at Mach Number from 1.57 to 2.86 PDF Author: Dennis E. Fuller
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38

Get Book Here

Book Description

Aerodynamics of Tactical Weapons to Mach Number 8 and Angle of Attack 180°

Aerodynamics of Tactical Weapons to Mach Number 8 and Angle of Attack 180° PDF Author: Leroy Devan
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics).
Languages : en
Pages : 192

Get Book Here

Book Description