[PDF] Jet Blast Attenuation For Super Boosters - eBooks Review

Jet Blast Attenuation For Super Boosters


Jet Blast Attenuation For Super Boosters
DOWNLOAD

Download Jet Blast Attenuation For Super Boosters PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Jet Blast Attenuation For Super Boosters book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page



Jet Blast Attenuation For Super Boosters


Jet Blast Attenuation For Super Boosters
DOWNLOAD
Author : Charles Alfred Anderson
language : en
Publisher:
Release Date : 1961

Jet Blast Attenuation For Super Boosters written by Charles Alfred Anderson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Attenuation (Physics) categories.




Rocket Engine Jet Blast Attenuation In Water


Rocket Engine Jet Blast Attenuation In Water
DOWNLOAD
Author : Grady W. Leese
language : en
Publisher:
Release Date : 1967

Rocket Engine Jet Blast Attenuation In Water written by Grady W. Leese and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Rocket research categories.


The investigation was conducted to determine the feasibility of launching missiles and superboosters from overwater sites. Information is needed to predict the depth of liquid-propellant rocket engine exhaust gas penetration into water. Methods will be required to minimize the depth of blast penetration and the upward splash of water. Since these large vehicles will generate high levels of noise during static test firing or lift-off, some method of noise suppression is desired in order to control possible harmful conditions for working personnel and to limit the size of the required test or launch area. Overwater blast tests with small-scale rocket engines of 250-, 500-, and 1000-lb thrusts were conducted (a) without underwater devices, (b) with underwater screens, and (c) with an underwater deflecting device exhausting into a group of cylindrical screens. Based on the results of this study, the following conclusions are believed warranted: (a) The rocket engine exhaust blast-penetration tests show that a relation exists between height of engine above the water, engine thrust, and depth of blast penetration into the water. (b) Depth of blast penetration can be reduced by an underwater deflecting device. (c) Splash action and noise intensity can be reduced by the use of an underwater deflector which directs the exhaust into a number of horizontal concentric, cylindrical screens. (Author).



List Of Publications Of The Ohio River Division Laboratories


List Of Publications Of The Ohio River Division Laboratories
DOWNLOAD
Author : United States. Army. Corps of Engineers. Ohio River Division Laboratories
language : en
Publisher:
Release Date : 1962

List Of Publications Of The Ohio River Division Laboratories written by United States. Army. Corps of Engineers. Ohio River Division Laboratories and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with categories.




Airframe Powerplant Mechanics


Airframe Powerplant Mechanics
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 2023

Airframe Powerplant Mechanics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2023 with Airframes categories.




Scientific And Technical Aerospace Reports


Scientific And Technical Aerospace Reports
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1974

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aeronautics categories.


Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.



Fluid Dynamics Research On Supersonic Aircraft


Fluid Dynamics Research On Supersonic Aircraft
DOWNLOAD
Author : North Atlantic Treaty Organization. Research and Technology Organization
language : en
Publisher:
Release Date : 1998

Fluid Dynamics Research On Supersonic Aircraft written by North Atlantic Treaty Organization. Research and Technology Organization and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with Technology & Engineering categories.


Contains the lecture notes prepared for a Special Course on Fluid Dynamics Research on Supersonic Aircraft organized by the RTO Applied Vehicle Technology Panel (AVT). The Course was held at the von Kármán Institute for Fluid Dynamics (VKI) Institute, Rhode-Saint-Genèse, Belgium 25-29 May 1998. The following topics were covered: History & Economics of Supersonic Transports, Supersonic Aerodynamics, Sonic Boom Theory and Minimization, Multi-Point Design Challenges, Vortex Plume Interactions, Propulsion System Design. Presentations on the major world wide supersonic transport programs were also included. The material assembled in this publication was prepared under the combined sponsorship of the RTO Applied Vehicle Technology Panel, the Consultant and Exchange Program of RTO, and the von Kármán Institute (VKI) for Fluid Dynamics.



Effects On Adjacent Surfaces From The Firing Of Rocket Jets


Effects On Adjacent Surfaces From The Firing Of Rocket Jets
DOWNLOAD
Author : Walter E. Bressette
language : en
Publisher:
Release Date : 1957

Effects On Adjacent Surfaces From The Firing Of Rocket Jets written by Walter E. Bressette and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Charts, diagrams, etc categories.


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.



Shock Wave Boundary Layer Interactions


Shock Wave Boundary Layer Interactions
DOWNLOAD
Author : Holger Babinsky
language : en
Publisher: Cambridge University Press
Release Date : 2011-09-12

Shock Wave Boundary Layer Interactions written by Holger Babinsky and has been published by Cambridge University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2011-09-12 with Technology & Engineering categories.


Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.



Report Of The Presidential Commission On The Space Shuttle Challenger Accident


Report Of The Presidential Commission On The Space Shuttle Challenger Accident
DOWNLOAD
Author : DIANE Publishing Company
language : en
Publisher: DIANE Publishing
Release Date : 1995-07

Report Of The Presidential Commission On The Space Shuttle Challenger Accident written by DIANE Publishing Company and has been published by DIANE Publishing this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995-07 with categories.




W Rtsil Encyclopedia Of Ship Technology


W Rtsil Encyclopedia Of Ship Technology
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 2015

W Rtsil Encyclopedia Of Ship Technology written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2015 with Marine engineering categories.