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 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

Author	: Ross B. Robinson
Publisher	:
Total Pages	: 38
Release	: 1959
ISBN-10	: UIUC:30112106741272
ISBN-13	:
Rating	: 4/5 ( Downloads)

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Book Synopsis 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 by : Ross B. Robinson

Download or read book 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 written by Ross B. Robinson and published by . This book was released on 1959 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 Related Books

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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Language: en
Pages: 100

Investigation of Jet Plume Effects on the Longitudinal Stability Characteristics of a Body of Revolution with Various Fin Configurations at Mach Numbers from 0.2 to 2.3

Authors: James H. Henderson

Categories: Aerodynamics, Transonic

Type: BOOK - Published: 1976 - Publisher:

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Transonic wind tunnel tests were conducted on a body of revolution with various fin configurations to investigate jet plume effects on missile longitudinal stab

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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Language: en
Pages: 194

A Summary of Jet Plume Effects on the Stability Characteristics of a Body of Revolution with Various Fin Configurations at Mach Numbers from 0.2 to 2.3

Authors: George Batiuk

Categories: Guided missiles

Type: BOOK - Published: 1976 - Publisher:

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This report summarizes the studies made to date by the Army Missile Command on the effects of the rocket jet plume on the Stability characteristics of a body of

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