Author : Arthur L. Jones
Publisher :
Page : 78 pages
File Size : 36,5 MB
Release : 1949
Category : Aerofoils
ISBN :
The variations of lift and pitching moment with sideslip in supersonic flow have been calculated for a representative gorup of plan forms. The variations of lift and pitching moment with aspect ratio and Mach number at zero sideslip were also investigated. The analysis was based on linearized potential theory and was applied to triangular, trapezoidal, rectangular, and swept-back plan forms without dihedral.
Author : Richard E. Kuhn
Publisher :
Page : 50 pages
File Size : 11,30 MB
Release : 1955
Category : Aerodynamic load
ISBN :
Author : Cornelius Driver
Publisher :
Page : 56 pages
File Size : 35,3 MB
Release : 1959
Category : Aerodynamic measurements
ISBN :
Author : Arthur Leslie Jones
Publisher :
Page : 72 pages
File Size : 20,59 MB
Release : 1949
Category : Aerodynamics, Supersonic
ISBN :
The variation of the yawing moment with sideslip and the variation of the stability derivative with aspect ratio and Mach number were investigated.
Author : Arthur L. Jones
Publisher :
Page : 644 pages
File Size : 43,52 MB
Release : 1948
Category : Aerodynamics, Supersonic
ISBN :
The variation of the rolling moment with sideslip and the variation of the derivative with aspect ratio and Mach number were investigated.
Author : Edward Charles Polhamus
Publisher :
Page : 86 pages
File Size : 16,55 MB
Release : 1960
Category : Aerodynamics, Transonic
ISBN :
Author : Edward C. Polhamus
Publisher :
Page : 34 pages
File Size : 35,80 MB
Release : 1955
Category : Airplanes
ISBN :
Author : Edward C. Polhamus
Publisher :
Page : 90 pages
File Size : 32,14 MB
Release : 1955
Category : Aerodynamics
ISBN :
A summary and analysis has been made of results obtained in a systematic research program concerned with the effects of wing sweep, aspect ratio, taper ratio, and dihedral on the rolling moment due to sideslip characteristics of wing-fuselage configurations up to Mach numbers of about 0.95. Other test results are presented to show trends of rolling moment due to sideslip with Mach number for a few wings in the transonic and supersonic speed range.
Author :
Publisher :
Page : 420 pages
File Size : 34,92 MB
Release : 1987
Category : Astronautics
ISBN :
Author :
Publisher :
Page : 52 pages
File Size : 17,21 MB
Release : 1972
Category : Aeronautics
ISBN :
The naval aviation safety review.
