Aerodynamic And Cold Jet Plume Geometry Characteristics Of The Army Free Rocket At Transonic Mach Numbers

Author : E. S. Washington
Publisher :
ISBN 13 :
Total Pages : 142 pages
Book Rating : 4.36/5 ( download)

DOWNLOAD NOW!

Download or read book Aerodynamic and Cold Jet Plume Geometry Characteristics of the Army Free Rocket at Transonic Mach Numbers written by E. S. Washington and published by . This book was released on 1975 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : James H. Henderson
Publisher :
ISBN 13 :
Total Pages : 100 pages
Book Rating : 4.28/5 ( download)

DOWNLOAD NOW!

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).

Author : James H Henderson
Publisher :
ISBN 13 :
Total Pages : 148 pages
Book Rating : 4.76/5 ( download)

DOWNLOAD NOW!

Download or read book An Experimental Investigation Using a Normal Jet Plume Simulator to Determine Jet Plume Effects on a Long Slender Rocket Configuration at Mach Numbers from 0.2 to 1.5 written by James H Henderson and published by . This book was released on 1977 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental aerodynamic investigations were conducted at the AEDC 16-foot Transonic Wind Tunnel to determine longitudinal stability characteristics of a long slender rocket configuration with simulated jet plume. The effect of jet plume on rocket aerodynamics is given over an angle of attack range from -11 to 11 degrees at Mach numbers from 0.2 to 1.5. Plume simulator chamber pressure varied from 0 to 600 psia. Individual cruciform fin aerodynamic loads are also shown over the same ranges. (Author).

Author : George Batiuk
Publisher :
ISBN 13 :
Total Pages : 194 pages
Book Rating : 4.77/5 ( download)

DOWNLOAD NOW!

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.

Author :
Publisher :
ISBN 13 :
Total Pages : 1082 pages
Book Rating : 4.00/5 ( download)

DOWNLOAD NOW!

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1977 with total page 1082 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Albin O. Pearson
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.66/5 ( download)

DOWNLOAD NOW!

Download or read book Wind-tunnel Investigation at Mach Numbers from 0.60 to 1.20 of the Static Aerodynamic Characteristics of a Model of a Possible Nonlifting Reentry Capsule in Combination with a Rocket Booster written by Albin O. Pearson and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author :
Publisher :
ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.02/5 ( download)

DOWNLOAD NOW!

Download or read book Effects of Configuration Geometry on the Transonic Aerodynamic Characteristics of a Simulated Launch Vehicle written by and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Ross B. Robinson
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.72/5 ( download)

DOWNLOAD NOW!

Download or read book Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82 written by Ross B. Robinson and published by . This book was released on 1959 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Earl D. Knechtel
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.95/5 ( download)

DOWNLOAD NOW!

Download or read book Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4 written by Earl D. Knechtel and published by . This book was released on 1956 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted to determine the longitudinal aerodynamic characteristics at transonic speeds of missile configurations having three blunted cone-cylinder bodies. Modifications of the basic model were tested to indicate the effects of (a) relative lengths of coplanar bodies, (b) seals between the cylindrical portions of the bodies, (c) horizontal connecting surfaces near the rear of the bodies, and (d) triangular rather than coplanar body grouping. Lift, drag, and pitching-moment data were obtained at angles of attack from -4 to 12 degrees and Mach numbers from 0.6 to 1.4 for a constant Reynolds number of 5,500,000, based on average body length.

Author :
Publisher :
ISBN 13 :
Total Pages : 802 pages
Book Rating : 4.7K/5 ( download)

DOWNLOAD NOW!

Download or read book Government Reports Announcements written by and published by . This book was released on 1974 with total page 802 pages. Available in PDF, EPUB and Kindle. Book excerpt: