Slosh alleviator Patent
Slosh and swirl alleviator for liquid propellant tanks during transport and flight
Engineering topics
Publications and source records attributed to Nelson, W. J..
Slosh and swirl alleviator for liquid propellant tanks during transport and flight
Manned reentry vehicles soft landing aid by lift engines incorporated in design, discussing performance advantages
Manned reentry vehicles soft landing aid by lift engines incorporated in design, discussing performance advantages
Internal aerodynamics and performance of clustered jet-exit installations at transonic speeds
Explore the source record for details and available documents.
Explore the source record for details and available documents.
An investigation has been conducted on a full-scale model of the proposed XP-46 airplane in the N. A. C. A. full-scale wind tunnel pursuant to the request of the Amy Air Corps, Materiel Division. The primary purpose of the investigation was to determine the optimum arrangement of the various component parts to obtain the maximum high speed and to provide adequate engine cooling. Additional tests included a determination of the stalling characteristics and the effectiveness of ailerons and elevators. The profile drag of the wing was ascertained by the momentum method; the location of the transition point on the wing and the critical compressibility velocities of the various airplane components were determined from surface pressure surveys.