Proceedings Of Symposium On Aerothermoelasticity

Author : David M. Jones
Publisher : Unknown
Page : 1028 pages
File Size : 50,5 Mb
Release : 1962
Category : Aerodynamic heating
ISBN : UOM:39015095305168

Get Book

Proceedings of Symposium on Aerothermoelasticity by David M. Jones Pdf

A symposium on Aerothermoelasticity was held to present the latest significant developments in each scientific area and engineering area that comprise the component parts of this technology. New and significant contributions were presented in four technical areas consisting of dynamic aerothermoelasticity (flutter), stability and control, thermodynamics and aerodynamics (or aerothermodynamics), and structures including material and construction concepts. Categories important and significant to each technical area are discussed state-of-the-art wise. In addition, 26 separate papers are given on items of special importance.

Author : David M. Jones
Publisher : Unknown
Page : 1032 pages
File Size : 53,9 Mb
Release : 1962
Category : Aerodynamic heating
ISBN : OSU:32435004687414

Get Book

Proceedings of Symposium on Aerothermoelasticity by David M. Jones Pdf

A symposium on Aerothermoelasticity was held to present the latest significant developments in each scientific area and engineering area that comprise the component parts of this technology. New and significant contributions were presented in four technical areas consisting of dynamic aerothermoelasticity (flutter), stability and control, thermodynamics and aerodynamics (or aerothermodynamics), and structures including material and construction concepts. Categories important and significant to each technical area are discussed state-of-the-art wise. In addition, 26 separate papers are given on items of special importance.

Author : Anonim
Publisher : Unknown
Page : 800 pages
File Size : 41,9 Mb
Release : 1964
Category : Aeroelasticity
ISBN : UVA:X000940290

Get Book

Proceedings of Symposium on Aeroelastic & Dynamic Modeling Technology, 23-24-25 September 1963, Dayton, Ohio by Anonim Pdf

Author : Anonim
Publisher : Unknown
Page : 550 pages
File Size : 51,6 Mb
Release : 1962
Category : Government publications
ISBN : STANFORD:36105024705100

Get Book

Proceedings of the NASA-University Conference on the Science and Technology of Space Exploration by Anonim Pdf

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 992 pages
File Size : 50,7 Mb
Release : 1962
Category : Outer space
ISBN : IND:30000088883628

Get Book

Proceedings of the NASA-University Conference on the Science and Technology of Space Exploration, Chicago, Illinois, November 1-3, 1962 by United States. National Aeronautics and Space Administration Pdf

Author : Anonim
Publisher : Unknown
Page : 544 pages
File Size : 44,8 Mb
Release : 1962
Category : Astrophysics
ISBN : UOM:39015017572986

Get Book

Proceedings by Anonim Pdf

Author : Raymond L. Bisplinghoff,Holt Ashley
Publisher : Courier Corporation
Page : 554 pages
File Size : 55,8 Mb
Release : 2002-01-01
Category : Technology & Engineering
ISBN : 0486495000

Get Book

Principles of Aeroelasticity by Raymond L. Bisplinghoff,Holt Ashley Pdf

Summary and general methods of constructing static and dynamic equations, dealing with the laws of mechanics for heated elastic solids, forms of aerodynamic operators, structural operators, much more. 1962 edition.

Author : Chicago NASA - University Conference on the Science and Technology of Space Exploration
Publisher : Unknown
Page : 56 pages
File Size : 43,9 Mb
Release : 1963
Category : Space vehicles
ISBN : UVA:X004374041

Get Book

Structures for Space Operations by Chicago NASA - University Conference on the Science and Technology of Space Exploration Pdf

Author : Anonim
Publisher : Unknown
Page : 968 pages
File Size : 51,9 Mb
Release : 1971
Category : Aeronautics
ISBN : UOM:39015006099223

Get Book

NASA Technical Note by Anonim Pdf

Author : Sidney C. Dixon
Publisher : Unknown
Page : 40 pages
File Size : 45,9 Mb
Release : 1962
Category : Mach number
ISBN : UIUC:30112106743450

Get Book

Experimental Investigation at Mach Number 3.0 of Effects of Thermal Stress and Buckling on Flutter Characteristics of Flat Single-bay Panels of Length-width Ration 0.96 by Sidney C. Dixon Pdf

Author : Anonim
Publisher : Unknown
Page : 420 pages
File Size : 43,8 Mb
Release : 1973
Category : Gases
ISBN : STANFORD:36105000610258

Get Book

Proceedings of the ... Symposium on Thermophysical Properties by Anonim Pdf

Author : Anonim
Publisher : Unknown
Page : 556 pages
File Size : 45,5 Mb
Release : 1962
Category : Electronic
ISBN : NASA:31769000652092

Get Book

PROCEEDINGS OF THE NASA-UNIVERSITY CONFERENCE ON THE SCIENCE AND TECHNOLOGY OF SPACE EXPLORATION, VOLUME 2, CHICAGO, NOVEMBER 1-3, 1962 by Anonim Pdf

Author : NASA Symposium on Instability of Shell Structures
Publisher : Unknown
Page : 800 pages
File Size : 53,9 Mb
Release : 1962
Category : Elastic plates and shells
ISBN : UVA:X001400582

Get Book

Collected Papers on Instability of Shell Structures, 1962 by NASA Symposium on Instability of Shell Structures Pdf

Author : Ivan E. Beckwith,Frank L. Clark,William D. Harvey
Publisher : Unknown
Page : 100 pages
File Size : 53,5 Mb
Release : 1971
Category : Heat
ISBN : UIUC:30112106691964

Get Book

Comparisons of Turbulent-boundary-layer Measurements at Mach Number 19.5 with Theory and an Assessment of Probe Errors by Ivan E. Beckwith,Frank L. Clark,William D. Harvey Pdf

Measurements of total temperature and pitot pressure across boundary layer of test section wall of axisymmetric contoured nozzle at hypersonic speed in nitrogen.

Author : Paul Czysz
Publisher : Unknown
Page : 116 pages
File Size : 41,7 Mb
Release : 1963
Category : Hypersonic wind tunnels
ISBN : UOM:39015095317759

Get Book

The High-Temperature Hypersonic Gasdynamics Facility Estimated Mach Number 6 Through 14 Performance by Paul Czysz Pdf

The High Temperature Gas Dynamics Facility was developed as a result of the Aeronautical Systems Division's effort to extend the state-of the-art in hypersonic aerodynamic simulation. The facility is a hypersonic wind tunnel supplied with high pressure air, heated from a zirconia dioxide pebble heater. The maximum stagnation pressure and temperature is 40 atres and 4700 R, respectively. This facility is one of four of its kind in this hemisphere and the only Air Force facility of its type. This report discusses the modification of the facility to a two foot diameter test section with a Mach number range of 6 through 14 and its expected performance. This facility is scheduled to be operational in the Fall of 1963.