Add to ORKGDesign curves are presented which permit rapid estimations of lift and pitching moment for given values of aspect ratio, taper ratio, Mach number, and leading-edge sweep.Based upon time-dependent linearized supersonic flow, theoretical approximations of lift and pitching moment produced by constant vertical accelerations were derived for a series of sweptback tapered wings with streamwise tips. The results are applicable for a range of Mach number for which the wing is wholly contained between the Mach cones springing from the nose and apex of the trailing edge of the wing.NACA TN No. 2315."March 1951."Includes bibliographical references.Design curves are presented which permit rapid estimations of lift and pitching moment for given values ...
Lift, pitching-moment, and pressure distribution were measured on a wing which was swept -40, -30, 0...
The effect of various wing geometry parameters on lift generation at supersonic speeds has been stud...
Measured values of lift, drag, and pitching moment at M(sub o) = 1.53 are presented for seven wings ...
Design curves are presented which permit rapid estimation of the lift-curve slope and damping-in-rol...
On the basis of linearized supersonic-flow theory, generalized equations were derived and calculatio...
A method is presented for determining the rolling and yawing moments of swept-back wings in steady s...
The theoretical lift and pitching moment due to angle of attack and pitching and the lateral force a...
On the basis of linearized-supersonic-flow theory, the lateral force and yawing moment due to combin...
"July 28, 1952."Includes bibliographical references (p. 7-8).Mode of access: Internet
On the basis of linearized supersonic-flow theory, generalized equations were derived and calculatio...
"Januayr 12, 1952."Includes bibliographical references (p. 7).Mode of access: Internet
By the method of superposition of conical flows, the load distribution is calculated for regions of ...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
The variations of lift and pitching moment with sideslip in supersonic flow have been calculated for...
The results of a wind-tunnel investigation are presented which show the effect of the variation of t...
Lift, pitching-moment, and pressure distribution were measured on a wing which was swept -40, -30, 0...
The effect of various wing geometry parameters on lift generation at supersonic speeds has been stud...
Measured values of lift, drag, and pitching moment at M(sub o) = 1.53 are presented for seven wings ...
Design curves are presented which permit rapid estimation of the lift-curve slope and damping-in-rol...
On the basis of linearized supersonic-flow theory, generalized equations were derived and calculatio...
A method is presented for determining the rolling and yawing moments of swept-back wings in steady s...
The theoretical lift and pitching moment due to angle of attack and pitching and the lateral force a...
On the basis of linearized-supersonic-flow theory, the lateral force and yawing moment due to combin...
"July 28, 1952."Includes bibliographical references (p. 7-8).Mode of access: Internet
On the basis of linearized supersonic-flow theory, generalized equations were derived and calculatio...
"Januayr 12, 1952."Includes bibliographical references (p. 7).Mode of access: Internet
By the method of superposition of conical flows, the load distribution is calculated for regions of ...
This report presents the results of an investigation to ascertain the lift, drag, and pitching momen...
The variations of lift and pitching moment with sideslip in supersonic flow have been calculated for...
The results of a wind-tunnel investigation are presented which show the effect of the variation of t...
Lift, pitching-moment, and pressure distribution were measured on a wing which was swept -40, -30, 0...
The effect of various wing geometry parameters on lift generation at supersonic speeds has been stud...
Measured values of lift, drag, and pitching moment at M(sub o) = 1.53 are presented for seven wings ...