Solution investigated by EWR (Entwicklungsring Sued, Munich, West Germany) required engines to be installed in rotatable wing tip pods; basic investigations on VTOL projects with thrust modulation include simulation test with original engines, and simulation with PA CE 231 R computer which investigates complete flight regime from hovering to normal aerodynamic flight and consists of computer and fixed pilot seat with instrumentation similar to that of airplane; results obtained.
Contribution to problem of VTOL-control by thrust modulation
AIAA -- Tech Papers
Simulation for Aerospace Flight Conference ; 1963 VTOL-STOL
1963
8 pages
Aufsatz (Konferenz)
Englisch
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VTOL -- Composite or vectored thrust
Engineering Index Backfile | 1962
|Lift/thrust engines for VTOL aircraft
Engineering Index Backfile | 1961