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Blom, G.

Publications and source records attributed to Blom, G..

3 records
All sourcesNASA NTRSDOE OSTI
NASA NTRS1986

Viscous vortical flow calculations over delta wings

Two approaches to calculate turbulent vortical flows over delta wing configurations are illustrated. The first is for a simple delta wing at low speeds using the boundary layer approximation to treat the effects of the secondary separation. The second is for the supersonic case of a generic fighter using the NASA Ames parabolized Navier/Stokes method. Test/theory comparisons are given in both cases.

Blom, G.↗
NASA NTRS1986

PN/S calculations for a fighter W/F at high-lift yaw conditions

The NASA/Ames parabolized Navier/Stokes computer code was used to calculate the turbulent flow over the wing/fuselage for a generic fighter at M = 2.2. 18 deg angle-of-attack, and 0 and 5 deg yaw. Good test/theory agreement was achieved in the zero yaw case. No test data were available for the yaw case.

Wai, J. C.↗