Minimum wave drag at low supersonic speeds for wing-body combinations with fixed fore and aft portions of the fuselage and given total volume
By: E. E. Groth.
Contributors: Northrop Corporation. Norair Division
Publisher: Northrop Corporation, Norair Division
Published: 1960
Place of publication: Hawthorne, Calif
Number of pages: 26
Notes: Bibliographical references: p. 21.