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Author : L. W. Sims
Publisher :
ISBN 13 :
Total Pages : 162 pages
Book Rating : 4.3/5 (91 download)
Download or read book Analytical and Experimental Investigation of Supersonic Parachute Phenomena written by L. W. Sims and published by . This book was released on 1963 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Rodney Orval Bailey
Publisher :
ISBN 13 :
Total Pages : 222 pages
Book Rating : 4.:/5 (193 download)
Download or read book Analytical and Experimental Investigation of Sensitivity to Mach Number of the Mass Flow and Flow Field Properties of the Supersonic Guide Surface Parachute written by Rodney Orval Bailey and published by . This book was released on 1963 with total page 222 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Earl C. Myers
Publisher :
ISBN 13 :
Total Pages : 432 pages
Book Rating : 4.3/5 (91 download)
Download or read book Symposium on Parachute Technology and Evaluation written by Earl C. Myers and published by . This book was released on 1964 with total page 432 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : H. Ronald Miller
Publisher :
ISBN 13 :
Total Pages : 144 pages
Book Rating : 4.:/5 (135 download)
Download or read book An Analytical and Experimental Investigation of Supersonic Flow Over an Electrostatically Charged Wedge written by H. Ronald Miller and published by . This book was released on 1962 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 488 pages
Book Rating : 4.3/5 (91 download)
Download or read book Proceedings of Retardation and Recovery Symposium written by and published by . This book was released on 1963 with total page 488 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report contains the proceedings of the Retardation and Recovery Symposium sponsored by the Aeronautical Systems Division on 13 and 14 November 1962. The Introductory Session was opened with the Keynote Address which reviewed the use and applications of deployable aerodynamic decelerators throughout the past fifty (50) years and noted the areas in which additional work had to be accomplished. The four Technical Sessions deal with the latest significant developments in the retardation and recovery area. The Technical Sessions begin with presentations and discussions of investigations in the hypersonic and supersonic flight regimes followed by a technical analysis of transonic and supersonic flow phenomena. In addition, new aerodynamic decelerator designs and discussion of the wind tunnel tests pertaining to these designs, as well as overall reliability of recovery systems, are presented. The final Technical Session concludes with a discussion of the military, scientific, and general objectives for decelerators intended for future use.
Author :
Publisher :
ISBN 13 :
Total Pages : 826 pages
Book Rating : 4.:/5 (327 download)
Download or read book Report written by and published by . This book was released on 1963 with total page 826 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Nickolai Charczenko
Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (317 download)
Download or read book Wind-tunnel Investigation of Drag and Stabili- Ty of Parachutes at Supersonic Speeds written by Nickolai Charczenko and published by . This book was released on 1964 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher :
ISBN 13 :
Total Pages : 944 pages
Book Rating : 4.3/5 (91 download)
Download or read book Report written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and published by . This book was released on 1963 with total page 944 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 142 pages
Book Rating : 4.:/5 (227 download)
Download or read book THEORETICAL PARACHUTE INVESTIGATIONS. written by and published by . This book was released on 1961 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: Investigation of wake effects on the behavior of parachutes and other retardation devices behind large bodies at subsonic and supersonic speeds Investigatiion of basic stability parameters of conventional parachutes Theoretical study of supersonic parachute phenomena Theoretical analysis of the dynamics of theopening parachute Statistical analysis of extraction time, deployment time, opening time, and drag coefficient for aerial delivery parachutes and systems Gliding aerodynamic decelerator Effective porosity studies Study of flow patterns of aerodynamic decelerators by means of the surface wave analogy Stress analysis of the T-10 Troop Parachute.
Author : L. W. Sims
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.:/5 (54 download)
Download or read book Evolution of the Hyperflo Parachute written by L. W. Sims and published by . This book was released on with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Analytical and experimental studies of the characteristics of supersonic parachutes and associated phenomena, which resulted in the development of the Hyperflo parachute, are described. Data from wind tunnel test programs which were conducted with six and eight inch parachute models are discussed. These programs covered the Mach number range from 1.5 to 4.65 and included approximately 200 test conditions. The present paper describes the evolution of parachute canopies which performed satisfactorily through Mach 4.65 and, in a succeeding series of wind tunnel tests, through Mach 6. Results of a rocket sled test program and a free-flight program to test full-scale Hyperflo parachutes up to Mach numbers of 4.0 and altitudes of 130,000 feet are summarized.
Author :
Publisher :
ISBN 13 :
Total Pages : 1118 pages
Book Rating : 4.0/5 ( download)
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1964 with total page 1118 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Earl C. Myers
Publisher :
ISBN 13 :
Total Pages : 856 pages
Book Rating : 4.X/5 ( download)
Download or read book Proceedings written by Earl C. Myers and published by . This book was released on 1964 with total page 856 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. Federal Aviation Administration
Publisher :
ISBN 13 :
Total Pages : 590 pages
Book Rating : 4.3/5 (91 download)
Download or read book Selected Technical Reports written by United States. Federal Aviation Administration and published by . This book was released on 1963 with total page 590 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Helmut G. Heinrich
Publisher :
ISBN 13 :
Total Pages : 78 pages
Book Rating : 4.:/5 (227 download)
Download or read book Theoretical Parachute Investigations written by Helmut G. Heinrich and published by . This book was released on 1961 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: Investigation of wake effects on the behavior of parachutes and other retardation devices behind large bodies; Investigation of basic stability parameters of conventional parachutes; Theoretical study of supersonic parachute phenomena; Theoretical analysis of the dynamics of the opening parachute; Statistical analysis of extraction time, deployment time, opening time, and drag coefficient for aerial delivery parachutes and systems; Gliding aerodynamic decelerator; Effective porosity studies; Study of flow patterns of aerodynamic decelerators by means of the surface wave analogy; Stress analysis of the T-10 troop parachute; Aerodynamic characteristics of the parachute stabilized A-21 cargo container; Aerodynamic characteristics of the cross and wagon-wheel type parachutes; Determination of mass flow through parachutes with inherent geometric porosity.
Author : Charles A. Babish (III.)
Publisher :
ISBN 13 :
Total Pages : 118 pages
Book Rating : 4.3/5 (91 download)
Download or read book Visualization of the Flow Field about Parachute Canopy Models and Approximation of Canopy Pressure Distributions written by Charles A. Babish (III.) and published by . This book was released on 1965 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation of the flow field about rigid two-dimensional models of parachute canopies was conducted. Models representing the inflated profile shapes of the drag-producing surface of nine parachute canopy types were tested in the Air Force Institute of Technology (AFIT) Smoke Tunnel Test Facility. Angles of attack varied from 0 to 30 degrees and photographs of the models and attendant smoke stream patterns were obtained for each test condition.
Author : United States. National Aeronautics and Space Administration
Publisher :
ISBN 13 :
Total Pages : 792 pages
Book Rating : 4.F/5 ( download)
Download or read book Research and Technology Program Digest written by United States. National Aeronautics and Space Administration and published by . This book was released on with total page 792 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Leland W. Sims
Publisher :
ISBN 13 :
Total Pages : 218 pages
Book Rating : 4.3/5 (91 download)
Download or read book The Effects of Design Parameters and Local Flow Fields on the Performance of Hyperflo Supersonic Parachutes and High Dynamic Pressure Parachute Concepts written by Leland W. Sims and published by . This book was released on 1965 with total page 218 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wake flow field surveys were conducted in the wind tunnel behind several side strut mounted forebodies in the Mach number range from 2 to 5. Studies of the effects of design parameters on Hyperflo supersonic parachutes, and of high dynamic pressure parachute configurations deployed in such wakes were performed. Wake pressure distributions indicated an asymmetry due to the forebody support structure, and a disturbance to the flow field which emanates from the support structure. The latter was most pronounced at Mach numbers above 3. Modification to the wake caused by an air bleed into the forebody base was also indicated. Normal, but higher than predicted axial wake Mach number distributions were found to exist in the forebody wakes. Hyperflo tests at Mach numbers 5 to 5.5 showed abnormally large parachute oscillations with models located at large downstream positions aft of the forebodies. The effects of Hyperflo design parameters and forebody type on model performance are only qualitatively indicated by the tests conducted. (Author).
