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Author : Oasis
Publisher : Unknown
Page : 0 pages
File Size : 54,8 Mb
Release : 2023-05-25
Category : Rock musicians
ISBN : 1472285476
The first-ever authorised book from Oasis, one of the biggest bands on the planet.[Bokinfo].
Author : United States. Flight Standards Service
Publisher : Unknown
Page : 136 pages
File Size : 48,7 Mb
Release : 1961
Category : Supersonic transport planes
ISBN : RUTGERS:39030039860418
Author : Franklin Moore
Publisher : Unknown
Page : 756 pages
File Size : 40,9 Mb
Release : 1950
Category : Aerodynamics, Supersonic
ISBN : STANFORD:36105024795861
First-order relations were obtained for attenuation of shock and flow deflection outward along the shock. These relations probably conform closely to physical fact, provided the entrance slope is small. These relations contain an error, but become exact as the radial coordinate approaches inifinity. The error is thus probably of the second order over the entire shock front.
Author : C. W. Chiang,Richard D. Wagner (Jr.)
Publisher : Unknown
Page : 44 pages
File Size : 41,8 Mb
Release : 1970
Category : Aerodynamics, Supersonic
ISBN : UIUC:30112106880047
Author : D. Adamson,E. A. Bonney,I. D. V. Faro
Publisher : Unknown
Page : 366 pages
File Size : 42,5 Mb
Release : 1961
Category : Aerodynamics, Supersonic
ISBN : UOM:39015104955268
Author : Mikhail Grigorʹevich Kotik
Publisher : Unknown
Page : 228 pages
File Size : 46,7 Mb
Release : 1969
Category : Aerodynamics, Supersonic
ISBN : UIUC:30112105136318
Author : Edward J. Ray,Robert T. Taylor
Publisher : Unknown
Page : 84 pages
File Size : 48,6 Mb
Release : 1966
Category : Aerodynamics, Transonic
ISBN : UIUC:30112106659847
Author : Douglas R. Lord,K. R. Czarnecki
Publisher : Unknown
Page : 18 pages
File Size : 42,6 Mb
Release : 1955
Category : Aerodynamic load
ISBN : UOM:39015086507020
Author : Jerome B. Hammack
Publisher : Unknown
Page : 682 pages
File Size : 47,8 Mb
Release : 1952
Category : Aerodynamics, Supersonic
ISBN : STANFORD:36105024831591
The aerodynamic design of propellers from considerations of centrifugal force is presented. A solution is obtained for the span wise distribution of cross-sectional area required to attain constant centrifugal stress over most of the blade.
Author : Robert T. Taylor
Publisher : Unknown
Page : 22 pages
File Size : 46,5 Mb
Release : 1961
Category : Aerodynamics, Supersonic
ISBN : UIUC:30112106914879
An investigation was made in the Langley Unitary Plan wind tunnel to determine the behavior of paraglider models at moderate to high supersonic speeds. The models were deployed from a sting in the supersonic stream and steady-state aerodynamics performance data were obtained. Maximum values of the lift-drag ratio were about 1.4 at a Mach number of 2.65 and about 1.2 at a Mach number of 4.65. The angles of attack over which the models could be flown were limited by unsteady behavior of the canopy.
Author : Domenic J. Maglieri,Harvey H. Hubbard
Publisher : Unknown
Page : 28 pages
File Size : 53,8 Mb
Release : 1961
Category : Aeronautics
ISBN : UIUC:30112106872804
Author : Alexander J. Smits,Jean-Paul Dussauge
Publisher : Springer Science & Business Media
Page : 418 pages
File Size : 53,9 Mb
Release : 2006-05-11
Category : Science
ISBN : 9780387263052
A good understanding of turbulent compressible flows is essential to the design and operation of high-speed vehicles. Such flows occur, for example, in the external flow over the surfaces of supersonic aircraft, and in the internal flow through the engines. Our ability to predict the aerodynamic lift, drag, propulsion and maneuverability of high-speed vehicles is crucially dependent on our knowledge of turbulent shear layers, and our understanding of their behavior in the presence of shock waves and regions of changing pressure. Turbulent Shear Layers in Supersonic Flow provides a comprehensive introduction to the field, and helps provide a basis for future work in this area. Wherever possible we use the available experimental work, and the results from numerical simulations to illustrate and develop a physical understanding of turbulent compressible flows.
Author : K. R. Czarnecki
Publisher : Unknown
Page : 20 pages
File Size : 45,8 Mb
Release : 1966
Category : Aerodynamics, Supersonic
ISBN : UIUC:30112106776351
Author : Arthur E. Franklin,Robert M. Lust
Publisher : Unknown
Page : 164 pages
File Size : 48,6 Mb
Release : 1960
Category : Drag (Aerodynamics)
ISBN : UIUC:30112104458028
Author : Hermann J. Schaefer
Publisher : Unknown
Page : 24 pages
File Size : 50,6 Mb
Release : 1968
Category : Galactic cosmic rays
ISBN : UOM:39015095156983
The prospect of large-scale commercial passenger transportation at SST altitudes in the lower stratosphere calls for an accurate assessment of the galactic radiation exposure. Highest radiation levels prevail at high latitudes (polar region) and solar minimum and reach about 1 millirem/hour at 65,000 feet. The accumulated dose of 0.6 rem/year which an SST crew member spending 600 hours/year at altitude would receive exceeds the Maximum Permissible Dose (MPD) for 'Members of the Public' and would classify crew members as 'Radiation Workers' in terms of official recommendations. The assumption of 50 SST each exposing 200 passengers to 1000 hours/year at SST altitude would lead to a population dose about equal to the contribution from industrial radiation workers, with both exposures ranking well below the two largest man-made additions to the natural background, medical use of x-rays and fallout. The heavy flux is attenuated to 3 per cent or less at 65,000 feet, depending on the nuclear species; yet, only 0.1 per cent of this residual flux accounts for maximum ionization hits. That means the microbeam hazard of heavy nuclei is insignificant at SST altitudes. (Author).