Author: George Batiuk
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 194
Book Description
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
Author: George Batiuk
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 194
Book Description
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.
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 194
Book Description
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.
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
Author: James H. Henderson
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 100
Book Description
Transonic wind tunnel tests were conducted on a body of revolution with various fin configurations to investigate jet plume effects on missile longitudinal stability. A series of cold air normal jets located downstream of the base were utilized to simulate the jet plume. Fins of various planform geometry were tested at a forward longitudinal location only. The angle of attack range was -4 to 11 degrees at Mach numbers of from 0.2 to 2.3. The test was run at the Arnold Engineering Development Center Transonic (16T) and Supersonic (16S) wind tunnels and was designated AEDC SF172/TF360. (Author).
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 100
Book Description
Transonic wind tunnel tests were conducted on a body of revolution with various fin configurations to investigate jet plume effects on missile longitudinal stability. A series of cold air normal jets located downstream of the base were utilized to simulate the jet plume. Fins of various planform geometry were tested at a forward longitudinal location only. The angle of attack range was -4 to 11 degrees at Mach numbers of from 0.2 to 2.3. The test was run at the Arnold Engineering Development Center Transonic (16T) and Supersonic (16S) wind tunnels and was designated AEDC SF172/TF360. (Author).
Scientific and Technical Aerospace Reports
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)
Author: James H Henderson
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 356
Book Description
The main purpose of the report is to discuss some known available transonic flow approximate treatments and their applicabilities, including their limitations. This may suggest the possible future improvement of efforts in this renewed field. (Author).
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 356
Book Description
The main purpose of the report is to discuss some known available transonic flow approximate treatments and their applicabilities, including their limitations. This may suggest the possible future improvement of efforts in this renewed field. (Author).
Government reports annual index
Government Reports Announcements & Index
Comparison of Jet Plume Shape Predictions and Plume Influence on Sonic Boom Signature
Author: Raymond L. Barger
Publisher:
ISBN:
Category : Jets
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Jets
Languages : en
Pages : 28
Book Description
Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85
Author: Reino J. Salmi
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 26
Book Description
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 26
Book Description