Download Full eBooks in PDF
Results Of Full Scale Wind Tunnel Tests On The H 126 Jet Flap Aircraft 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 Results Of Full Scale Wind Tunnel Tests On The H 126 Jet Flap Aircraft book. This book definitely worth reading, it is an incredibly well-written.
Author : Anthony M. Cook,Dale G. Jones
Publisher : Unknown
Page : 66 pages
File Size : 44,6 Mb
Release : 1969
Category : Jet flaps (Airplanes)
ISBN : UIUC:30112106595819
Author : Anonim
Publisher : Unknown
Page : 94 pages
File Size : 41,7 Mb
Release : 1975
Category : Electronic
ISBN : NASA:31769000531106
Author : Anonim
Publisher : Unknown
Page : 410 pages
File Size : 47,6 Mb
Release : 1973
Category : Electronic
ISBN : MINN:319510008464540
Author : Paul T. Soderman,Thomas N. Aiken
Publisher : Unknown
Page : 108 pages
File Size : 49,9 Mb
Release : 1971
Category : Airplanes
ISBN : UIUC:30112106692574
The aerodynamic characteristics of a full scale executive type jet transport aircraft with a T-tail were investigated in a 40 x 80 ft (12.2 by 24.4 meter) wind tunnel (subsonic). Static, longitudinal, and lateral stability, and control characteristics were determined at angles of attack from -2 deg to 42 deg. The aircraft wing had 13 deg of sweep and an aspect ratio of 5.02. The aircraft was tested power off with various wing leading- and trailing-edge high lift devices. The basic configuration was tested with and without such components as engine nacelles, wing tip tanks, and empannage. Hinge-moment data were obtained and downwash angles in the horizontal-tail plane location were calculated. The data were obtained at Reynolds numbers of 4.1 million and 8.7 million based on mean aerodynamic chord. The model had static longitudinal stability through initial stall. Severe tail buffet occurred near the angle of attack for maximum lift. Above initial stall the aircraft had pronounced pitch-up, characteristic of T-tail configurations. A stable trim point was possible at angles of attack between 30 deg and 40 deg (depending on c.g. location and flap setting). Hinge-moment data showed no regions with adverse effects on stick force. Comparisons of wind-tunnel data and flight-test are presented.
Author : Anonim
Publisher : Unknown
Page : 126 pages
File Size : 42,9 Mb
Release : 1975
Category : Aeronautics, Military
ISBN : UIUC:30112104133027
Author : United States. Naval Air Systems Command
Publisher : Unknown
Page : 122 pages
File Size : 47,7 Mb
Release : 1975
Category : Aeronautics, Military
ISBN : CORNELL:31924071765667
Author : Anonim
Publisher : Unknown
Page : 952 pages
File Size : 49,7 Mb
Release : 1987
Category : Aeronautics
ISBN : UIUC:30112075701505
Author : Anonim
Publisher : Unknown
Page : 1064 pages
File Size : 45,7 Mb
Release : 2010
Category : Aeronautics
ISBN : UCSD:31822036341212
Two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, historians, museum curators, journalists, and independent scholars. Explores various aspects of how NACA-NASA research took aeronautics from the subsonic to the hypersonic era.-publisher description.
Author : Anonim
Publisher : Unknown
Page : 1066 pages
File Size : 41,5 Mb
Release : 2011
Category : Electronic
ISBN : STANFORD:36105050567168
Author : Kiyoshi Aoyagi
Publisher : Unknown
Page : 64 pages
File Size : 55,6 Mb
Release : 1963
Category : Airplanes
ISBN : UIUC:30112106597450
Author : David H. Hickey,Kiyoshi Aoyagi
Publisher : Unknown
Page : 56 pages
File Size : 50,5 Mb
Release : 1960
Category : Aerodynamics
ISBN : UIUC:30112106588806
Author : Mark W. Kelly,William H. Tolhurst,Ralph L. Maki
Publisher : Unknown
Page : 28 pages
File Size : 42,5 Mb
Release : 1959
Category : Trailing edge flaps
ISBN : UIUC:30112106742437
Author : Lysle P. Parlett,Delma C. Freeman,Charles Christian Smith
Publisher : Unknown
Page : 84 pages
File Size : 44,8 Mb
Release : 1970
Category : Jet transports
ISBN : UIUC:30112106880989
Author : Richard K. Grief,William H. Tolhurst
Publisher : Unknown
Page : 112 pages
File Size : 42,6 Mb
Release : 1963
Category : Jet planes
ISBN : UIUC:30112106872929
Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 792 pages
File Size : 42,9 Mb
Release : 2024-07-02
Category : Electronic
ISBN : STANFORD:36105112109157