Zobrazeno 1 - 3
of 3
pro vyhledávání: '"Nathan W. Graybeal"'
Publikováno v:
Journal of Aircraft. 50:1716-1725
The effects of engine placement and sweep on the flutter characteristics of an aft-swept flying wing resembling the Horten IV are investigated using the Nonlinear Aeroelastic Trim and Stability of HALE Aircraft. The analysis was validated against the
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
A data acquisition system was developed for the recording of flight test data of a Cessna 172 S general aviation aircraft. The proposed system required the ability to reliably acquire data suitable for a validation database for general aviation simul
Publikováno v:
AIAA Guidance, Navigation, and Control Conference and Exhibit.
A simp le model for the dynamic response of an inflatable solar sailcraft during deployment has been developed and tested for several distinct scenarios. The basic kinematics for the model were formulated in a deliberate manner that in future studies