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supersonic airfoils

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View Supersonic wing and wing-body shape optimization using an adjoint formulation By James Reuther

Supersonic wing and wing-body shape optimization using an adjoint formulation

Supersonic wing and wing-body shape optimization using an adjoint formulation

By James Reuther

View Delta wings with shock-free cross flow By S. S. Sritharan

Delta wings with shock-free cross flow

Delta wings with shock-free cross flow

By S. S. Sritharan

View Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16 By Richard M. Wood

Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16

Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16

By Richard M. Wood

View Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰ By M. Leroy Spearman

Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰

Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰

By M. Leroy Spearman

View Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1 By M. Khalid

Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1

Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1

By M. Khalid