Normal-force and Pitching-moment Characteristics for Two Blunt-nosed Re-entry Type Bodies from M

Normal-force and Pitching-moment Characteristics for Two Blunt-nosed Re-entry Type Bodies from M
Title Normal-force and Pitching-moment Characteristics for Two Blunt-nosed Re-entry Type Bodies from M PDF eBook
Author Charles E. DeRose
Publisher
Pages 14
Release 1959
Genre
ISBN

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Some Measurements of the Dynamic and Static Stability of Two Blunt-nosed, Low-fineness-ratio Bodies of Revolution in Free Flight at M

Some Measurements of the Dynamic and Static Stability of Two Blunt-nosed, Low-fineness-ratio Bodies of Revolution in Free Flight at M
Title Some Measurements of the Dynamic and Static Stability of Two Blunt-nosed, Low-fineness-ratio Bodies of Revolution in Free Flight at M PDF eBook
Author Barbara J. Sort
Publisher
Pages 34
Release 1959
Genre Angle of attack (Aerodynamics)
ISBN

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Measurements of the Flow Over Blunt-nosed Bodies at Mach Numbers from 2.5 to 3.5

Measurements of the Flow Over Blunt-nosed Bodies at Mach Numbers from 2.5 to 3.5
Title Measurements of the Flow Over Blunt-nosed Bodies at Mach Numbers from 2.5 to 3.5 PDF eBook
Author Joseph L. Frank
Publisher
Pages 62
Release 1960
Genre
ISBN

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STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG

STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG
Title STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG PDF eBook
Author
Publisher
Pages 48
Release 1959
Genre
ISBN

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Some Measurements of the Dynamic and Static Stability of Two Blunt-nosed, Low-fineness- Ratio Bodies of Revolution in Free Flight at Mequal4

Some Measurements of the Dynamic and Static Stability of Two Blunt-nosed, Low-fineness- Ratio Bodies of Revolution in Free Flight at Mequal4
Title Some Measurements of the Dynamic and Static Stability of Two Blunt-nosed, Low-fineness- Ratio Bodies of Revolution in Free Flight at Mequal4 PDF eBook
Author
Publisher
Pages 34
Release 1959
Genre
ISBN

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NASA Technical Memorandum

NASA Technical Memorandum
Title NASA Technical Memorandum PDF eBook
Author
Publisher
Pages 396
Release 1959
Genre Aeronautics
ISBN

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The Damping in Pitch of Bluff Bodies of Revolution at Mach Numbers from 2.5 to 3.5

The Damping in Pitch of Bluff Bodies of Revolution at Mach Numbers from 2.5 to 3.5
Title The Damping in Pitch of Bluff Bodies of Revolution at Mach Numbers from 2.5 to 3.5 PDF eBook
Author
Publisher
Pages 36
Release 1959
Genre
ISBN

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