Making Sense of Census 2000
Author :
Publisher :
Page : 8 pages
File Size : 20,12 MB
Release : 1999
Category : United States
ISBN :
Of Interest to Visitors
Author :
Publisher :
Page : 2 pages
File Size : 32,32 MB
Release : 1999
Category : Hoosier National Forest (Ind.)
ISBN :
Book Description
U.S. Government Subscriptions
Author :
Publisher :
Page : 134 pages
File Size : 39,70 MB
Release : 2003
Category : Booksellers' catalogs
ISBN :
Book Description
Simulator Study of Stall/post-stall Characteristics of a Fighter Airplane with Relaxed Longitudinal Static Stability
Author :
Publisher :
Page : 236 pages
File Size : 30,22 MB
Release : 1979
Category :
ISBN :
Book Description
Senate Treaty Documents
Author :
Publisher : Government Printing Office
Page : 1028 pages
File Size : 10,5 MB
Release : 1986
Category : United States
ISBN :
Book Description
A Parametric Study of the Aerodynamic Characteristics of Nose-cylinder-flare Bodies at a Mach Number of 6.0
Author : George C. Ashby
Publisher :
Page : 82 pages
File Size : 42,54 MB
Release : 1965
Category : Aerodynamics, Hypersonic
ISBN :
Book Description
Summary of Flight-test Results of the VZ-2 Tilt-wing Aircraft
Author : Robert J. Pegg
Publisher :
Page : 48 pages
File Size : 47,11 MB
Release : 1962
Category : Aerodynamics
ISBN :
Book Description
Flutter of Flat Rectangular Orthotropic Panels with Biaxial Loading and Arbitrary Flow Direction
Author : Herman L. Bohon
Publisher :
Page : 48 pages
File Size : 19,55 MB
Release : 1963
Category : Aerodynamics, Supersonic
ISBN :
Book Description
Buckling of a Pressurized Toroidal Ring Under Uniform External Loading
Author : George E. Weeks
Publisher :
Page : 28 pages
File Size : 36,8 MB
Release : 1967
Category : Buckling (Mechanics)
ISBN :
Book Description
Investigation of Engine-exhaust-airframe Interference on a Cruise Vehicle at Mach 6
Author : James M. Cubbage
Publisher :
Page : 76 pages
File Size : 15,2 MB
Release : 1971
Category : Aircraft exhaust emissions
ISBN :
Book Description
Results from an investigation of the effects of underexpanded engine exhaust flow on the aerodynamic performance and stability of a cruise airplane at Mach 6 are presented. The influence of wing reflex angle and nozzle geometry on exhaust flow interference effects was investigated on a flat-plate model. The experiments were conducted at a free-stream Reynolds number of 17.05 X 10 (to the 6 power) based on the length of the airplane model over a model angle-of-attack range of 0(degrees) to 10(degrees) and at nozzle static-pressure ratios from 1 to approximately 4.
