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A Preliminary Analysis Of Rocket Exhaust Jet Effects On Missile Skin And Base Pressures At Mach 06 And 15 Naca Lewis Flight Propulsion Laboratory Test 2093
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Book Synopsis A Preliminary Analysis of Rocket Exhaust Jet Effects on Missile Skin and Base Pressures at Mach 0.6 and 1.5 - Naca Lewis Flight Propulsion Laboratory Test 2093 by : G. E. Powell
Download or read book A Preliminary Analysis of Rocket Exhaust Jet Effects on Missile Skin and Base Pressures at Mach 0.6 and 1.5 - Naca Lewis Flight Propulsion Laboratory Test 2093 written by G. E. Powell and published by . This book was released on 1958 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind tunnel test of a one-thirtieth scale 'B' series Atlas missile with operating rocket engines was run at the NACA Lewis 8-by-6 foot supersonic wind tunnel. The primary test objective was to determine the amount of rocket and gas turbine exhaust recirculation into the missile base region; a secondary objective was to determine the effect of operating rockets on missile skin and base pressure. Only the pressure data are considered in this report. (Author).
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 850 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects on Adjacent Surfaces from the Firing of Rocket Jets by : Walter E. Bressette
Download or read book Effects on Adjacent Surfaces from the Firing of Rocket Jets written by Walter E. Bressette and published by . This book was released on 1957 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85 by : Reino J. Salmi
Download or read book Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85 written by Reino J. Salmi and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : James H. Henderson
Download or read book 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 written by James H. Henderson and published by . This book was released on 1976 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).
Book Synopsis 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 by : William F. Hinson
Download or read book 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 written by William F. Hinson and published by . This book was released on 1967 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : George Batiuk
Download or read book 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 written by George Batiuk and published by . This book was released on 1976 with total page 194 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Jet Effects at Supersonic Speeds on Base and Afterbody Pressures of a Missile Model Having Single and Multiple Jets by : Nickolai Charczenko
Download or read book Jet Effects at Supersonic Speeds on Base and Afterbody Pressures of a Missile Model Having Single and Multiple Jets written by Nickolai Charczenko and published by . This book was released on 1963 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some Observations of Base Heating at Mach 3.0 on a Simulated Missile with JP-4 Liquid-oxygen Rocket by : Nick E. Samanich
Download or read book Some Observations of Base Heating at Mach 3.0 on a Simulated Missile with JP-4 Liquid-oxygen Rocket written by Nick E. Samanich and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Simulated Rocket-jet Exhaust on Stability and Control of a Research-type Airplane Configuration at Mach Number of 6.86 by : David E. Fetterman
Download or read book Effects of Simulated Rocket-jet Exhaust on Stability and Control of a Research-type Airplane Configuration at Mach Number of 6.86 written by David E. Fetterman and published by . This book was released on 1959 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Close-range Rocket-exhaust Impingement on Surfaces in a Vacuum by : Leonard V. Clark
Download or read book Experimental Investigation of Close-range Rocket-exhaust Impingement on Surfaces in a Vacuum written by Leonard V. Clark and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Rocket Plume Effects on Boattail and Flare Bodies of Revolution at Transonic Speeds by : Donald V. Rubin
Download or read book Rocket Plume Effects on Boattail and Flare Bodies of Revolution at Transonic Speeds written by Donald V. Rubin and published by . This book was released on 1971 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report presents an analysis of the pressure data from a wind tunnel test conducted to gain information about rocket plume effects on missile base pressure and local pressure along flared and boattailed bodies of revolution at transonic speeds. The jet plume was simulated by a cold air jet over a pressure range from 0 to approximately 600 psia. (Author).
Author :Frederick S. Simmons Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 : Total Pages :312 pages Book Rating :4.3/5 (91 download)
Book Synopsis Rocket Exhaust Plume Phenomenology by : Frederick S. Simmons
Download or read book Rocket Exhaust Plume Phenomenology written by Frederick S. Simmons and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 2000 with total page 312 pages. Available in PDF, EPUB and Kindle. Book excerpt: This new book deals with the phenomenology of rocket exhaust plumes as the targets of space-based surveillance systems. Topics include the physical and chemical processes in rocket engines and their exhaust plumes, particularly in regard to flow properties, gas dynamics, and radiative mechanisms that are responsible for the generation of emission in rocket exhaust plumes at infrared and other wavelengths. System designers in a number of defense-related areas will be able to put the information in this book to immediate use.
Book Synopsis Effects of Simulated Rocket-jet Exhaust on Stability and Control of a Research-type Airplane Configuration at a Mach Number of 6.86 by : David E. Jr Fetterman
Download or read book Effects of Simulated Rocket-jet Exhaust on Stability and Control of a Research-type Airplane Configuration at a Mach Number of 6.86 written by David E. Jr Fetterman and published by . This book was released on 1959 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure Distribution Induced on a Flat Plate at a Free-stream Mach Number of 1.39 by Rockets Exhausting Upstream and Downstream by : Abraham Leiss
Download or read book Pressure Distribution Induced on a Flat Plate at a Free-stream Mach Number of 1.39 by Rockets Exhausting Upstream and Downstream written by Abraham Leiss and published by . This book was released on 1962 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Base Heating and Rocket Hinge Moments for a Simulated Missile Through a Mach Number Range of 0.8 to 2.0 by : Bruce G. Chiccine
Download or read book Experimental Investigation of Base Heating and Rocket Hinge Moments for a Simulated Missile Through a Mach Number Range of 0.8 to 2.0 written by Bruce G. Chiccine and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Measured Base Pressures on Several Twin Rocket-nozzle Configurations at Mach Nubmers of 0.6 to 1.4 with Effects Due to Nozzle Canting and Stabilizing Fins by : James M. Cubbage
Download or read book Measured Base Pressures on Several Twin Rocket-nozzle Configurations at Mach Nubmers of 0.6 to 1.4 with Effects Due to Nozzle Canting and Stabilizing Fins written by James M. Cubbage and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
