1. Slender-Body Theory-Review and Extension
2. During Simulated Launching from the Midsemispan and Wing-Tip Locations of a 45° Sweptback Wing-FuselageCombination," RM L55A12, April 1955, NACA.
3. namic Forces and Moments at High Subsonic Speeds on a Missile Model During Simulated Launching from the Midsemispan Location of a 45° Sweptback Wing-Fuselage-Pylon Combination," RM L56J05, Jan. 1957, NACA.