An Investigation to Determine the Stability Characteristics of Three Supersonic-impact Ballistic Reentry Shapes at Mach Numbers from 1.2 to 4.2

An Investigation to Determine the Stability Characteristics of Three Supersonic-impact Ballistic Reentry Shapes at Mach Numbers from 1.2 to 4.2
Title An Investigation to Determine the Stability Characteristics of Three Supersonic-impact Ballistic Reentry Shapes at Mach Numbers from 1.2 to 4.2 PDF eBook
Author
Publisher
Pages 52
Release 1962
Genre
ISBN

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Experimental Investigation of Pressure Distribution and Static Aerodynamic Characteristics for Three Supersonic Impact Ballistic Reentry Shapes at Mach Numbers of 1.93, 2.55, and 3.05

Experimental Investigation of Pressure Distribution and Static Aerodynamic Characteristics for Three Supersonic Impact Ballistic Reentry Shapes at Mach Numbers of 1.93, 2.55, and 3.05
Title Experimental Investigation of Pressure Distribution and Static Aerodynamic Characteristics for Three Supersonic Impact Ballistic Reentry Shapes at Mach Numbers of 1.93, 2.55, and 3.05 PDF eBook
Author
Publisher
Pages 44
Release 1961
Genre
ISBN

Download Experimental Investigation of Pressure Distribution and Static Aerodynamic Characteristics for Three Supersonic Impact Ballistic Reentry Shapes at Mach Numbers of 1.93, 2.55, and 3.05 Book in PDF, Epub and Kindle

Static Stability Investigation of Supersonic-impact Ballistic Reentry Shapes at Mach Numbers of 2.55 and 3.05

Static Stability Investigation of Supersonic-impact Ballistic Reentry Shapes at Mach Numbers of 2.55 and 3.05
Title Static Stability Investigation of Supersonic-impact Ballistic Reentry Shapes at Mach Numbers of 2.55 and 3.05 PDF eBook
Author John M. Swihart
Publisher
Pages 16
Release 1959
Genre
ISBN

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Experimental Investigation of Pressure Distribution and Static Aerodynamic Characteristics for Three Supersonic Impact Ballistic Reentry Shapes at Mach Number of 1.93, 2.55 and 3.05

Experimental Investigation of Pressure Distribution and Static Aerodynamic Characteristics for Three Supersonic Impact Ballistic Reentry Shapes at Mach Number of 1.93, 2.55 and 3.05
Title Experimental Investigation of Pressure Distribution and Static Aerodynamic Characteristics for Three Supersonic Impact Ballistic Reentry Shapes at Mach Number of 1.93, 2.55 and 3.05 PDF eBook
Author Odell A. Morris
Publisher
Pages 40
Release 1961
Genre
ISBN

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An Exploratory Investigation in a Ballistic Range of the Stability Derivatives of a Simple Airplane Configuration at Low Supersonic Speeds

An Exploratory Investigation in a Ballistic Range of the Stability Derivatives of a Simple Airplane Configuration at Low Supersonic Speeds
Title An Exploratory Investigation in a Ballistic Range of the Stability Derivatives of a Simple Airplane Configuration at Low Supersonic Speeds PDF eBook
Author Charles E. DeRose
Publisher
Pages 30
Release 1959
Genre Aerodynamics, Supersonic
ISBN

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Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87

Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87
Title Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87 PDF eBook
Author Donald T. Gregory
Publisher
Pages 36
Release 1959
Genre Stability of airplanes, Longitudinal
ISBN

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Title Scientific and Technical Aerospace Reports PDF eBook
Author
Publisher
Pages 992
Release 1974
Genre Aeronautics
ISBN

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