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 Download

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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

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

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 :
Languages : en
Pages : 67

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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 : 46

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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 on Adjacent Surfaces from the Firing of Rocket Jets

Effects on Adjacent Surfaces from the Firing of Rocket Jets PDF Author: Walter E. Bressette
Publisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 14

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Book Description
This paper is a preliminary and brief account of some research currently being conducted to determine the jet effects on adjacent surfaces from the firing of rocket jets. Measurements of jet-effect pressures on a flat plate as well as shadowgraphs are presented that were obtained when a rocket jet at a Mach number of 3 was exhausted downstream and upstream into free-stream flow at a Mach number of 2 located from 2 to 4.7 rocket-jet-exit diameters from the plate. The jet effects on the flat plate with the rocket jet exhausting downstream are of the same order of magnitude as those previously obtained from sonic exits with a total pressure 10 times lower. A maximum pressure coefficient on the plate of 1.35 was obtained when the rocket jet was exhausted upstream at 2 rocket-jet-exit diameters below the plate, and an integration of the measured jet-effect pressures at this position resulted in a normal force on the plate equal to 2.3 times the thrust output of the rocket jet.

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

Effects of Canted Forward Faces on the Static Longitudinal Stability Characteristics of the Escape and Exit Configurations of a Project Mercury Capsule Model at a Mach Number of 2.01

Effects of Canted Forward Faces on the Static Longitudinal Stability Characteristics of the Escape and Exit Configurations of a Project Mercury Capsule Model at a Mach Number of 2.01 PDF Author: Roy V. Harris
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 24

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Book Description

Pressure Distribution Induced on a Flat Plate at a Free-stream Mach Number of 1.39 by Rockets Exhausting Upstream and Downstream

Pressure Distribution Induced on a Flat Plate at a Free-stream Mach Number of 1.39 by Rockets Exhausting Upstream and Downstream PDF Author: Abraham Leiss
Publisher:
ISBN:
Category :
Languages : en
Pages : 58

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Book Description

Static Stability Investigation of a Single-stage Sounding Rocket at Mach Numbers from 0.60 to 1.20

Static Stability Investigation of a Single-stage Sounding Rocket at Mach Numbers from 0.60 to 1.20 PDF Author: James C. Ferris
Publisher:
ISBN:
Category : Sounding rockets
Languages : en
Pages : 68

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Book Description

Fundamentals of Rocket Propulsion

Fundamentals of Rocket Propulsion PDF Author: DP Mishra
Publisher: CRC Press
ISBN: 1351708414
Category : Technology & Engineering
Languages : en
Pages : 364

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Book Description
The book follows a unified approach to present the basic principles of rocket propulsion in concise and lucid form. This textbook comprises of ten chapters ranging from brief introduction and elements of rocket propulsion, aerothermodynamics to solid, liquid and hybrid propellant rocket engines with chapter on electrical propulsion. Worked out examples are also provided at the end of chapter for understanding uncertainty analysis. This book is designed and developed as an introductory text on the fundamental aspects of rocket propulsion for both undergraduate and graduate students. It is also aimed towards practicing engineers in the field of space engineering. This comprehensive guide also provides adequate problems for audience to understand intricate aspects of rocket propulsion enabling them to design and develop rocket engines for peaceful purposes.