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References from ACTIVE VORTICAL FLOW CONTROL FOR ALLEVIATION OF TWIN-TAIL BUFFET OF GENERIC FIGHTER AIRCRAFT. Local targets link to admitted publications; unresolved targets remain external evidence.
Effects of spanwise blowing on two fighter airplane configurations
10.2514/3.57980 · 1980 · External reference
10.2514/6.1997-1090
10.2514/6.1997-1090 · External reference
Unresolved reference
External reference
Unresolved reference
External reference
10.2514/6.1997-621
10.2514/6.1997-621 · External reference
10.2514/6.1995-3440
10.2514/6.1995-3440 · External reference
Unresolved reference
External reference
10.1006/jfls.1998.0168
10.1006/jfls.1998.0168 · External reference
10.2514/6.1996-2517
10.2514/6.1996-2517 · External reference
10.2514/6.1997-2261
10.2514/6.1997-2261 · External reference
10.2514/6.1999-138
10.2514/6.1999-138 · External reference
10.2514/6.1998-4738
10.2514/6.1998-4738 · External reference
10.2514/6.1990-1432
10.2514/6.1990-1432 · External reference
Vortical-flow structure near the F/A-18 LEX at high incidence
10.2514/3.46636 · 1994 · External reference
Unresolved reference
External reference
Unresolved reference
External reference
Effects of blowing on delta wing vortices during dynamic pitching
10.2514/3.46339 · 1993 · External reference
10.2514/6.1998-1957
10.2514/6.1998-1957 · External reference
10.2514/6.1992-2673
10.2514/6.1992-2673 · External reference
Performance augmentation of a 60-degree delta aircraft configuration by spanwise blowing
10.2514/3.45384 · 1986 · External reference
10.4271/881448
10.4271/881448 · External reference
10.2514/6.1991-2889
10.2514/6.1991-2889 · External reference
Unresolved reference
External reference
Unresolved reference
External reference
10.2514/6.1999-792
10.2514/6.1999-792 · External reference
10.2514/6.1998-5501
10.2514/6.1998-5501 · External reference
Unresolved reference
External reference
Unresolved reference
External reference
Unresolved reference
1998 · External reference
10.2514/6.1993-50
10.2514/6.1993-50 · External reference
10.2514/6.1987-2474
10.2514/6.1987-2474 · External reference
Active control of wing rock using tangential leading-edge blowing
10.2514/3.46545 · 1994 · External reference
Control of vortical lift on delta wings by tangential leading-edge blowing
10.2514/3.45583 · 1988 · External reference
