Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85 PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85 PDF full book. Access full book title Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85 by Reino J. Salmi. Download full books in PDF and EPUB format.

Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85

Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85 PDF Author: Reino J. Salmi
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 26

Get Book Here

Book Description

Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85

Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85 PDF Author: Reino J. Salmi
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 26

Get Book Here

Book Description

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 PDF Author: George Batiuk
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 194

Get Book Here

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

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 PDF Author: James H. Henderson
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 100

Get Book Here

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).

Effects of Simulated Rocket-jet Exhaust on Stability and Control of a Research-type Airplane Configuration at Mach Number of 6.86

Effects of Simulated Rocket-jet Exhaust on Stability and Control of a Research-type Airplane Configuration at Mach Number of 6.86 PDF Author: David E. Fetterman
Publisher:
ISBN:
Category : Stability of airplanes
Languages : en
Pages : 46

Get Book Here

Book Description

Some Effects of Jet Pluming on the Static Stability of Ballistic Bodies at a Mach Number of 6.00

Some Effects of Jet Pluming on the Static Stability of Ballistic Bodies at a Mach Number of 6.00 PDF Author: Robert J. McGhee
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36

Get Book Here

Book Description

Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0

Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0 PDF Author: J. T. Best (Jr.)
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 194

Get Book Here

Book Description
Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the High Altitude Supersonic Target (HAST) missile.

Investigation of Static Stability and Aerodynamic Effects of Control Jets on a 1/3-scale Pye Wacket Missile at Transonic Mach Numbers

Investigation of Static Stability and Aerodynamic Effects of Control Jets on a 1/3-scale Pye Wacket Missile at Transonic Mach Numbers PDF Author: D. C. BAKER
Publisher:
ISBN:
Category :
Languages : en
Pages : 49

Get Book Here

Book Description

Effects of Simulated Rocket-jet Exhaust on Stability and Control of a Research-type Airplane Configuration at a Mach Number of 6.86

Effects of Simulated Rocket-jet Exhaust on Stability and Control of a Research-type Airplane Configuration at a Mach Number of 6.86 PDF Author: David E. Jr Fetterman
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

Get Book Here

Book Description

AN EXPERIMENTAL INVESTIGATION OF THE INTERFERENCE EFFECTS DUE TO A LATERAL JET ISSUING FROM A BODY OF REVOLUTION OVER THE MACH NUMBER RANGE OF 0.8 TO 4.5

AN EXPERIMENTAL INVESTIGATION OF THE INTERFERENCE EFFECTS DUE TO A LATERAL JET ISSUING FROM A BODY OF REVOLUTION OVER THE MACH NUMBER RANGE OF 0.8 TO 4.5 PDF Author: Donald J. Spring
Publisher:
ISBN:
Category :
Languages : en
Pages : 110

Get Book Here

Book Description

Effects of Simulated Rocket-jet Exhaust on Stability and Control of a Research-type Airplane Configuration at Mach Number of 6.86

Effects of Simulated Rocket-jet Exhaust on Stability and Control of a Research-type Airplane Configuration at Mach Number of 6.86 PDF Author: David E. Fetterman
Publisher:
ISBN:
Category : Stability of airplanes
Languages : en
Pages : 35

Get Book Here

Book Description