Drag and stability derivatives of missile components according to the modified Newtonian theory
By: J. Don Gray.
Contributors: Arnold Engineering Development Center
Publisher: Arnold Engineering Development Center, Air Research and Development Command, United States Air Force
Published: 1960
Place of publication: [Arnold Air Force Station, Tenn.]
Number of pages: 36
Notes: ARO project no. 300116.

Bibliographical references: p. 23.

Contract number: AF-40(600)-800-S/A-11(60-110)