FFA TN / Flygtekniska Försöksanstalten

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Bibliographische Detailangaben
Körperschaft: Flygtekniska Försöksanstalten (VerfasserIn)
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Sprache:eng
Veröffentlicht: Stockholm FFA 1985-
Schlagworte:
Monografische Reihe > Forschungsbericht
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Titel Jahr Band
Multiaxial fatigue : a literature survey 2000
Dynamic stall and three-dimensional effects : final report for the EC DGXII Joule II project JOU2-CT93-0345 1996
Flap efficiency for a double delta wing : results from tests with the Greta model in the Mach number range M=0.70 - 7.15 Suppl. 2 Surface flow visualization 1993 Suppl. 2
Flap efficiency for a double delta wing : results from tests with the Greta model in the Mach number range M=0.70 - 7.15 [Hauptbd.] 1993 [Hauptbd.]
Flap efficiency for a double delta wing : results from tests with the Greta model in the Mach number range M=0.70 - 7.15 Suppl. 1 Total force and moment measurements 1993 Suppl. 1
Impact response of composite laminates : a guide to closed form solutions 1992
On missing boundary conditions with unsteady incompressible Navier-Stokes flows 1990
Eurovisc annual report 18.1989 1989 18.1989
Three-dimensional inviscid turbomachinery flow simulations obtained by solving the Euler equations on an O-H type grid 1986
Grid generation for compressor/turbine configurations 1986
Eurovisc annual report 1984 1985 1984
An experimental investigation of supersonic flow over axisymmetric afterbodies with a centered propulsive jet at angles of attack 1985
The flow field about a hemisphere-cylinder body at a Mach number of 7.3 1962
An experimental and theoretical investigation of second-order wing-body interference at high Mach number 1962
Second-order theory for a thin wing in supersonic flow with a weak spanwise entropy grandient 1961
An experimental and theoretical investigation of second-order supersonic wing-body interference, for an on-lifting body with wings at incidence 1960
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