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Effects Of Simulated Retrorockets On The Aerodynamic Characteristics Of A Body Of Revolution At Mach Numbers From 025 To 190

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Effects of Simulated Retrorockets on the Aerodynamic Characteristics of a Body of Revolution at Mach Numbers from 0.25 to 1.90
Language: en
Pages: 50

Effects of Simulated Retrorockets on the Aerodynamic Characteristics of a Body of Revolution at Mach Numbers from 0.25 to 1.90

Authors: Victor L. Peterson
Categories: Aerodynamics
Type: BOOK - Published: 1962 - Publisher:

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Effects of Simulated Retrorockets on the Aerodynamic Characteristics of a Body of Revolution at Mach Numbers from 0.25 to 1.90
Language: en
Pages: 45

Effects of Simulated Retrorockets on the Aerodynamic Characteristics of a Body of Revolution at Mach Numbers from 0.25 to 1.90

Authors: Victor L. Peterson
Categories:
Type: BOOK - Published: 1962 - Publisher:

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Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82
Language: en
Pages: 38

Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82

Authors: Ross B. Robinson
Categories: Mach number
Type: BOOK - Published: 1959 - Publisher:

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Static Aerodynamic Characteristics of Three Rocket-vehicle Configurations at Mach Numbers from 1.80 to 4.63 Including Some Effects of Fin Size, Fin Cant, and Auxiliary Rocket Motors
Language: en
Pages: 64

Static Aerodynamic Characteristics of Three Rocket-vehicle Configurations at Mach Numbers from 1.80 to 4.63 Including Some Effects of Fin Size, Fin Cant, and Auxiliary Rocket Motors

Authors: Dennis E. Fuller
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1963 - Publisher:

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An Investigation of Flow and Stability Characteristics for a Body of Revolution with Fins and Flare in Presence of Plume Induced Separation at Mach Numbers 0.7 to 1.4
Language: en
Pages: 200

An Investigation of Flow and Stability Characteristics for a Body of Revolution with Fins and Flare in Presence of Plume Induced Separation at Mach Numbers 0.7 to 1.4

Authors: Calvin Wayne Dahlke
Categories: Guided missiles
Type: BOOK - Published: 1977 - Publisher:

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The results of a wind tunnel test, simulating rocket motor exhaust jet effects on missile aerodynamic at Mach numbers of 0.7 to 1.4 are presented. A normal jet