Stability derivatives of triangular wings at supersonic speeds /

The analysis of the stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds in NACA TN No. 1423 is extended to triangular wings having larger vertex angles and traveling at supersonic speeds. Fifteen longitudinal and lateral derivatives, including the work of others, are presented with respect to both body axes and stability axes. Results are limited to Mach numbers for which the triangle is within the Mach cone.NACA TN No. 1572."May 1948."Includes bibliographical references.The analysis of the stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds in NACA TN No. 1423 is extended to triangular wings having larger vertex angles and traveling at supersonic speeds. Fifteen longitudinal and lateral derivatives, including the work of others, are presented with respect to both body axes and stability axes. Results are limited to Mach numbers for which the triangle is within the Mach cone.Mode of access: Internet