Measurement Problems in Research on Unstable Combustion of Solid Rocket Propellants 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 Measurement Problems in Research on Unstable Combustion of Solid Rocket Propellants PDF full book. Access full book title Measurement Problems in Research on Unstable Combustion of Solid Rocket Propellants by H. B. MATHES. Download full books in PDF and EPUB format.
Author: H. B. MATHES
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Get Book Here
Book Description
Several measurement problems which have been encountered in a long-range U.S. Navy research program on solid propellant combustion instability are discussed. Topics included are: (a) behavior of several types of high-frequency response pressure gages, (b) difficulties in detecting high-frequency pressure oscillations, (c) techniques in recording and storing detected data, and (d) methods used in recovery and analysis of recorded data. (Author).
Author: H. B. MATHES
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Get Book Here
Book Description
Several measurement problems which have been encountered in a long-range U.S. Navy research program on solid propellant combustion instability are discussed. Topics included are: (a) behavior of several types of high-frequency response pressure gages, (b) difficulties in detecting high-frequency pressure oscillations, (c) techniques in recording and storing detected data, and (d) methods used in recovery and analysis of recorded data. (Author).
Author: Martin Summerfield
Publisher: Elsevier
ISBN: 0323163351
Category : Science
Languages : en
Pages : 713
Get Book Here
Book Description
Solid Propellant Rocket Research
Author: H. B. Mathes
Publisher:
ISBN:
Category :
Languages : en
Pages : 25
Get Book Here
Book Description
A review is presented of the classes of instability, conditions favoring each class, experimental measurements recognized to diagnose each class, and problems in conducting such measurements. (Author).
Author:
Publisher:
ISBN:
Category : Detonation waves
Languages : en
Pages : 1532
Get Book Here
Book Description
Author: Martin Summerfield
Publisher: AIAA
ISBN: 9781600863967
Category : Solid propellants
Languages : en
Pages : 922
Get Book Here
Book Description
Author: David T. Harrje
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 668
Get Book Here
Book Description
The solution of problems of combustion instability for more effective communication between the various workers in this field is considered. The extent of combustion instability problems in liquid propellant rocket engines and recommendations for their solution are discussed. The most significant developments, both theoretical and experimental, are presented, with emphasis on fundamental principles and relationships between alternative approaches.
Author: JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB.
Publisher:
ISBN:
Category :
Languages : en
Pages : 111
Get Book Here
Book Description
The paper, Experimental measurements of acoustic erosivity effects on propellant burning rates, by R.C. Strittmater, W.P. Aungst, C.E. Thompson and L.A. Watermeier, is given in its entirety. In addition, condensed versions of the following papers are included: Problems in liquid propellant instability; Liquid instability problems; An experimental study of solid propellant combustion instability in a standing wave tube; Basic physical processes of solid propellant combustion; Shock wave -- burning solid propellant interaction; Acoustic absorption coefficients of the combustion products of aluminized propellants; Further development of 'Stability grading of solid propellants by the oscillatory strand burner test'; An interpretive study of unstable rocket combustion data and method for the simulation of such data; Work at Summerfield Research Station and the University of Sheffield, England; Influence of compositional factors on axial instability; Influence of axial combustion instability on the development of a 23KS20000 motor; Progress in research on combustion instability of solid propellants at the University of Utah; Low frequency acoustic instability studies with double base propellants; Bulk compressibility of solid propellants; Solution of transient vibration problems by separation of variables.
Author: Vigor Young
Publisher: AIAA
ISBN: 9781600864186
Category : Liquid propellant rockets
Languages : en
Pages : 606
Get Book Here
Book Description
Annotation Since the invention of the V-2 rocket during World War II, combustion instabilities have been recognized as one of the most difficult problems in the development of liquid propellant rocket engines. This book is the first published in the United States on the subject since NASA's Liquid Rocket Combustion Instability (NASA SP-194) in 1972. In this book, experts cover four major subject areas: engine phenomenology and case studies, fundamental mechanisms of combustion instability, combustion instability analysis, and engine and component testing. Especially noteworthy is the inclusion of technical information from Russia and China--a first.
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 298
Get Book Here
Book Description
Author: P. C. Braithwaitet
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Get Book Here
Book Description
The problem of combustion instability in solid rocket propellants has been studied extensively over the past three decades. The most common way oscillatory combustion is controlled in rocket motors today is through the use of additives known as acoustic suppressants. The perfect suppressant would control all of the oscillatory modes which are present in a solid propellant rocket motor. Unfortunately suppressants that work well at one frequency, such as the product in a longitudinal mode, can be quite ineffective at other frequencies, such as tangential mode. Still, some suppressants have been relatively successful in suppressing oscillations in operational motors, the more successful suppressants include Al, ZrC and graphite.
