Effects of Centerbody Length and Nose Shape on the Transonic Characteristics of Low-fineness- Ratio Bodies of Revolution with a Flared Afterbody PDF Download

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Effects of Centerbody Length and Nose Shape on the Transonic Characteristics of Low-fineness- Ratio Bodies of Revolution with a Flared Afterbody

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Languages : en
Pages : 96

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Author:
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Languages : en
Pages : 96

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Effects of Nose-cone Angle on the Transonic Aerodynamic Characteristics of a Blunt Cone- Cylinder Body Having a Cylindrical, Flared, Or Blunt-finned Afterbody PDF

Author: Stuart L. Treon
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Languages : en
Pages : 64

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Languages : en
Pages : 508

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Effects of Spike-mounted Flow Deflectors on the Transonic Aerodynamic Characteristics of a Blunt-nosed Body of Revolution Having a Cylindrical Or Flared Afterbody PDF

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Languages : en
Pages : 56

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Effects of Configuration Geometry on the Transonic Aerodynamic Characteristics of a Simulated Launch Vehicle PDF

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Languages : en
Pages : 54

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An Empirical Method for Determining Static Distributed Aerodynamic Loads on Axisymmetric Multistage Launch Vehicles PDF

Author: Ralph John Muraca
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Category : Aerodynamic load
Languages : en
Pages : 114

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Transonic Static Aerodynamic Characteristics of a Low Fineness Ratio Body of Revolution Having a Blunt Allipsoidal Nose and Flared Afterbodies of Various Angles and Base Areas PDF

Author: Earl A. Knechtel
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Category :
Languages : en
Pages : 45

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Transonic Longitudinal Aerodynamic Characteristics of Five Cone Cylinder Flare Bodies of Revolution PDF

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Category :
Languages : en
Pages : 54

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Comparison of the Effectiveness of Flares with that of Fins for Stabilizing Low Fineness Ratio Bodies at Mach Numbers from 0.6 to 5.8 PDF

Author: Leland H. Jorgensen
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Languages : en
Pages : 40

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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

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Category :
Languages : en
Pages : 48

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