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Valter J. E. Stark
Observed names:
V. STARK,
VALTER J. E. STARK,
Valter J.E. Stark,
ValterI J. E. Stark
Observed institution:
Saab (Sweden)
OpenAlex ID:
A5091678291
Numerical lifting-surface theory - Problems and progress.
1968
·
MARTEN T. LANDAHL
, VALTER J. E. STARK
·
AIAA Journal
·
106
A generalized quadrature formula for Cauchy integrals
1971
·
VALTER J. E. STARK
·
AIAA Journal
·
32
General equations of motion for an elastic wing and method of solution
1984
·
Valter J. E. Stark
·
AIAA Journal
·
23
On the approximation of the normal velocity on oscillating wings.
1966
·
VALTER J. E. STARK
·
AIAA Journal
·
13
Canard-wing interaction in unsteady supersonic flow
1989
·
Valter J. E. Stark
·
Journal of Aircraft
·
7
Indicial coefficients for a cropped delta wing in incompressible flow
1986
·
Valter J. E. Stark
·
Journal of Aircraft
·
6
A flutter eigenvalue program based on the Newton-Raphson method
1984
·
Valter J.E. Stark
·
AIAA Journal
·
6
Applications at M = 1 of a method for solving the subsonic problem of the oscillating finite wing with the aid of high-speed digital computers
1964
·
Valter J. E. Stark
·
Springer eBooks
·
6
The tangent plane method and polar coordinates - A new approach in lifting-surface theory
1970
·
V. STARK
·
8th Aerospace Sciences Meeting
·
5
Measurement of derivatives for an oscillating airfoil with flap
1981
·
Valter J. E. Stark
·
Journal of Aircraft
·
4
Comparative flutter calculations for the Viggen aircraft
1977
·
Valter J. E. Stark
, Dale E. Cooley
·
Journal of Aircraft
·
4
Test of Pines' approximate method in a flutter calculation for the Viggen aircraft
1977
·
Valter J. E. Stark
·
Journal of Aircraft
·
4
Leading-edge vortex effect on the flutter speed
1977
·
Valter J. E. Stark
·
Journal of Aircraft
·
3
Use of complex cross-flow representation in nonplanar oscillating-surface theory.
1968
·
VALTER J. E. STARK
·
AIAA Journal
·
3
Comment on "Computation of Second-Order Accurate Unsteady Aerodynamic Generalized Forces"
1987
·
Valter J. E. Stark
·
AIAA Journal
·
2
Comment on "Induced Drag and Lift of Wing by the Piecewise Continuous Kernel Function Method"
1985
·
Valter J. E. Stark
·
Journal of Aircraft
·
2
General equations of motion for an elastic wing and method of solution
1983
·
V. STARK
·
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM)
·
2
A subsonic oscillating-surface theory for wings with partial-span controls
1972
·
V. STARK
·
10th Aerospace Sciences Meeting
·
2
Equivalence of damping from flight flutter test evaluation and eigenvalue calculation
1984
·
ValterI J. E. Stark
, Helmut Wittmeyer
·
Journal of Aircraft
Reply by Authors to S. Tsakonas
1969
·
MARTEN T. LANDAHL
, VALTER J. E. STARK
·
AIAA Journal
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Works count:
20
Citation count:
230
H-index:
6
I10-index:
4
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