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

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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

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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

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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

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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

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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 : 22

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Rocket-model Investigation of Lateral Stability Characteristics and Power Effects of a Jet-engine Airplane Configuration with Tail Boom at Mach Numbers from 1.15 to 1.37

Rocket-model Investigation of Lateral Stability Characteristics and Power Effects of a Jet-engine Airplane Configuration with Tail Boom at Mach Numbers from 1.15 to 1.37 PDF Author: T. Bradley Curry
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 34

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Book Description

Rocket-Model Investigation of Lateral Stability Characteristics and Power Effects of a Jet-Engine Airplane Configuration with Tail Boom at Mach Numbers from 1.15 to 1.37

Rocket-Model Investigation of Lateral Stability Characteristics and Power Effects of a Jet-Engine Airplane Configuration with Tail Boom at Mach Numbers from 1.15 to 1.37 PDF Author: T. Bradley Curry (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 29

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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

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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

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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 Jet Pluming on the Static Stability of Five Rocket Models at Mach Numbers of 4, 5, and 6 and Static Pressure Ratios Up to 26 000

Effects of Jet Pluming on the Static Stability of Five Rocket Models at Mach Numbers of 4, 5, and 6 and Static Pressure Ratios Up to 26 000 PDF Author: William F. Hinson
Publisher:
ISBN:
Category : Pitching (Aerodynamics)
Languages : en
Pages : 74

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Book Description

Controllability of the X-15 Research Airplane with Interim Engines During High-altitude Flights

Controllability of the X-15 Research Airplane with Interim Engines During High-altitude Flights PDF Author: Euclid C. Holleman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 28

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Book Description