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Application Of Transonic Area Rule To A Sharp Lipped Ducted Nacelle Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Application Of Transonic Area Rule To A Sharp Lipped Ducted Nacelle book. This book definitely worth reading, it is an incredibly well-written.
Author : Richard E. Walters
Publisher : Unknown
Page : 18 pages
File Size : 54,8 Mb
Release : 1954
Category : Aerodynamics, Transonic
ISBN : UOM:39015086465492
Author : Anonim
Publisher : Unknown
Page : 200 pages
File Size : 48,9 Mb
Release : 1961
Category : Aerodynamics
ISBN : MINN:30000011022005
Author : William E. Stoney
Publisher : Unknown
Page : 196 pages
File Size : 40,8 Mb
Release : 1961
Category : Body of revolution
ISBN : UIUC:30112106681353
This report presents a compilation of most of the zero-lift drag results obtained from free-flight measurements made by the Langley Pilotless Aircraft Research Division on fin-stabilized bodies of revolution. The data are arranged on standard forms, which also contain the significant geometrical factors. Supplementary data have been provided to facilitate the determination of the body pressure drags from the measurement total drags. Summary plots and discussions have been included to provide a unified and broad picture of the effects of the body geometry on zero-lift drag.
Author : Anonim
Publisher : Unknown
Page : 818 pages
File Size : 43,9 Mb
Release : 1954
Category : Aeronautics
ISBN : UVA:X004173286
Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 580 pages
File Size : 49,6 Mb
Release : 1956
Category : Aeronautics
ISBN : UCBK:C029901318
Author : Robert R. Howell
Publisher : Unknown
Page : 36 pages
File Size : 42,6 Mb
Release : 1954
Category : Aerodynamics, Supersonic
ISBN : UOM:39015086465690
Author : Defense Documentation Center (U.S.)
Publisher : Unknown
Page : 922 pages
File Size : 49,5 Mb
Release : 1960
Category : Industrial arts
ISBN : UOM:39015024208558
Author : Harold L. Crane
Publisher : Unknown
Page : 654 pages
File Size : 42,5 Mb
Release : 1958
Category : Airplanes
ISBN : STANFORD:36105024832391
A flight investigation at subsonic speeds of a method to improve the damping of lateral oscillations by means of a viscous damping cylinder used in the rudder system in conjunction with adjusted hinge-moment parameters has been conducted. The damping device has been applied to a modern fighter-type jet-powered airplane. The rudder was made to float with the relative wind by the addition of trailing-edge strips. In order to amplify the floating tendency (by reducing the restoring moment), a highly geared balancing tab was incorporated. Lag of the motion of the free rudder with respect to the yawing of the airplane was introduced by means of a small viscous damping cylinder linked to the rudder.
Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 1274 pages
File Size : 49,6 Mb
Release : 1958
Category : Aeronautics
ISBN : RUTGERS:39030037544691
Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 508 pages
File Size : 49,8 Mb
Release : 1954
Category : Aeronautics
ISBN : IND:30000098603164
Author : William E. Stoney (Jr.)
Publisher : Unknown
Page : 200 pages
File Size : 47,9 Mb
Release : 1961
Category : Electronic
ISBN : NASA:31769000421464
Author : Zbigniew Krzywoblocki (|d)
Publisher : Unknown
Page : 170 pages
File Size : 43,7 Mb
Release : 1957
Category : Aerodynamics
ISBN : UOM:39015095330323
Author : Joseph Adams Shortal
Publisher : Unknown
Page : 796 pages
File Size : 48,9 Mb
Release : 1978
Category : Aeronautics
ISBN : NASA:31769000524929
Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 128 pages
File Size : 44,7 Mb
Release : 1960-07
Category : Electronic
ISBN : STANFORD:36105024165701
Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 448 pages
File Size : 53,7 Mb
Release : 1960
Category : Aeronautics
ISBN : UIUC:30112032439504