Recently added
Login
AERADE Home
→
Aeronautical Research Council
→
Aeronautical Research Council (1945-1979)
→
Aeronautical Research Council Current Papers
→
Recent submissions
JavaScript is disabled for your browser. Some features of this site may not work without it.
Aeronautical Research Council Current Papers: Recent submissions
Now showing items 801-820 of 1393
Previous Page
Next Page
8 feet x 6 feet transonic wind tunnel tests on a .04 scale model of the fairey delta 2 (ER.103)
D. J. Kettle
(
1963
)
Propagation of fatigue cracks in wide unstiffened aluminium alloy sheets
K.D. Raithby
;
Marie E. Bebb
(
1963
)
Measurements of the moments of inertia of the avro 707B aircraft
D. H. Perry
(
1963
)
List of current papers (numbers 601-650)
Aeronautical Research Council
(
1964
)
A digital computer programme for the calculation of annular or two-dimensional supersonic potential flow in a duct by the method of characteristics
P. G. Street
(
1963
)
The calculation of optimum incidences for aerofoils
A. D. S. Carter
(
1961
)
Unsteady lift slope values obtained from flight measurements in gusts
D. M. Ridland
(
1963
)
Free-flight measurements of the dynamic longitudinal-stability characteristics of a wind tunnel interference model (M = 0.92 to 1.35)
G. H. Greenwood
(
1963
)
Measurements in flight of the longitudinal stability derivatives of a 60 degrees delta wing aircraft (Fairey Delta 2)
D.R. Andrews
(
1959
)
The effect of skin taper on the aeroelastic properties of wings
J. A. Rein
(
1961
)
Low speed wind tunnel tests on a kite balloon model
M. H. Simonds
(
1963
)
On axial load diffusion into a thin-walled reinforced cylindrical shell
E.H. Mansfield
(
1963
)
Non-equilibrium flow of a polyatomic gas through a normal shock wave
P. A. Blythe
(
1962
)
On Three-Dimensional Bodies of Delta Planform which can Support Plane Attached Shock Waves
D. H. Peckham
(
1963
)
This Note collects together in one report available theoretical work on bodies which can support attached plane shock waves, discusses some of the possible merits of such shapes, and includes some calculations illustrating ...
Pressure measurements at supersonic speeds on three uncambered conical wings of unit aspect ratio
J. W. Britton
(
1962
)
Three-dimensional turbulent boundary layers
J. C. Cooke
(
1963
)
Surface pressures and structural strains resulting from fluctuations in the turbulent boundary layer of a fairey delta 2 aircraft
D. R. B. Webb
;
A. R. Keeler
;
G. R. Allen
(
1962
)
Atomic recombination in nozzles methods of analysis for flows with complicated chemistry
K. N. C. Bray
;
J. P. Appleton
(
1963
)
Equilibrium real-gas performance charts for a hypersonic shock-tube wind-tunnel employing nitrogen
L. Bernstein
(
1963
)
Theoretical comparison of the flow over a flat delta wing and a rectangular pyramid
E. Eminton
(
1963
)
Now showing items 801-820 of 1393
Previous Page
Next Page
Search AERADE
Search AERADE
This Collection
Browse
All of AERADE
Communities & Collections
By Issue Date
Authors
Titles
Subjects
This Collection
By Issue Date
Authors
Titles
Subjects
My Account
Login