Recently added
Login
AERADE Home
→
Recent submissions
JavaScript is disabled for your browser. Some features of this site may not work without it.
AERADE: Recent submissions
Now showing items 2741-2760 of 3498
Previous Page
Next Page
Supersonic wind tunnel tests on a 1/12th scale model of the bristol type 188 research aircraft part 1 M = 1.4 to 2.0 part 2 M = 2.0 to 2.7
C. R. Taylor
;
T. A. Cook
(
1965
)
Alleviation of thermal stresses in aircraft structures
E. C. Capey
(
1965
)
Measurements of oscillatory derivatives at mach numbers up to 2.6 on a model of a supersonic transport design study (Bristol type 198)
J. S. Thompson
;
R. A. Fail
(
1965
)
Wind tunnel tests on a 1/12th scale model of the bristol type 188 research aircraft with rectangular, wedge intakes at mach numbers from 2.0 to 2.7
T. A. Cook
(
1965
)
Measurement of air temperature on an aircraft travelling at high subsonic and supersonic speeds
A. A. Woodfield
;
P. J. Haynes
(
1965
)
Measurements of skin-friction in an annulus by the floating element technique
J. K. White
;
R. E. Franklin
(
1965
)
Influence of chemical contouring on the fatigue and sustained load properties of high tensile steel sheet
Westland Aircraft Limited
;
Saunders-Roe Division
(
1965
)
Theoretical investigation of some basic assumptions of Schlichting's singularity method of cascade analysis
R. I. Lewis
;
G. A. Pennington
(
1965
)
The unsteady motion of slender wings with leading-edge vortices
B. D. Dore
(
1965
)
The chemical contouring of 3 percent chromium-molybdenum-vanadium and 5 percent chromium-molybdenum-vanadium high strength steel sheet
Bristol Aerojet Ltd
(
1965
)
Potential flow through cascades extensions to an exact theory
J. P. Gostelow
(
1965
)
Potential flow through cascades a comparison between exact and approximate solutions
J. P. Gostelow
(
1965
)
On the calculation of cascade flows
W. S. Hall
;
B. Thwaites
(
1965
)
Tests with a variable ramp intake having combined external/internal compression, and a design mach number of 2.2
M. C. Neale
;
P. S. Lamb
(
1965
)
Wind tunnel measurements of the far-field pressures due to some lifting, slender delta wings
T. A. Cook
(
1965
)
An experimental investigation into the determination of lift from wake traverses at supersonic speeds
J. Wooller
;
M.C.P. Firmin
(
1965
)
List of current papers (numbers 751-800)
Aeronautical Research Council
(
1965
)
Wind tunnel tests at mach numbers up to 2.80 to determine the effects of changing spanwise volume distribution on a slender, cambered ogee wing
T. A. Cook
(
1965
)
Wind tunnel measurements at mach numbers up to 2.80 of the effects of gulling on the longitudinal and lateral stability and drag of a cambered, slender ogee wing
T. A. Cook
(
1965
)
The steady flow of a viscous fluid past a circular cylinder
S. C. R. Dennis
;
M. Shimshoni
(
1965
)
Now showing items 2741-2760 of 3498
Previous Page
Next Page
Search AERADE
Browse
All of AERADE
Communities & Collections
By Issue Date
Authors
Titles
Subjects
My Account
Login