AEROX program estimates aircraft aerodynamics to high angles of attack (up to sixty degrees). It estimates coefficients of lift, induced drag, and pitching moment for wings and wing body combinations with or without aft horizontal tail. Both trimmed and untrimmed characters are calculated.
Aircraft aerodynamics at high angles of attack
NASA Tech Briefs ; 2 , 2
1977-09-01
Sonstige
Keine Angabe
Englisch
Aerodynamics forces on airfoils at high angles of attack
AIAA | 1988
|Aerodynamics of Slender Bodies at High Angles of Attack
NTIS | 1977
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