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

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
Author: George Batiuk
Publisher:
Total Pages: 194
Release: 1976
Genre: Guided missiles
ISBN:

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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 revolution with various fin configurations and at various fin positions on the body. The Mach numbers ranged from 0.2 to 2.3. A normal jet plume simulator was used to obtain the desired plume effects. This report concerns itself with those tests conducted on a 5-in. diameter, 52-in. long model, with a 3 caliber tangent ogive nose.


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
Language: en
Pages: 194
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
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
Language: en
Pages: 100
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
An Investigation of Jet Plume Effects on the Stability Characteristics of a Body of Revolution in Conjunction with Fins of Various Geometry and Longitudinal Positions at Transonic Speeds (sting-mounted Model with Normal Jet Plume Simulator)
Language: en
Pages: 356
Authors: James H Henderson
Categories: Aerodynamics, Transonic
Type: BOOK - Published: 1975 - Publisher:

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The main purpose of the report is to discuss some known available transonic flow approximate treatments and their applicabilities, including their limitations.
Scientific and Technical Aerospace Reports
Language: en
Pages: 1102
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1973 - Publisher:

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Scientific and Technical Aerospace Reports
Language: en
Pages: 684
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1974 - Publisher:

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