Investigation of Pitch Maneuver Speed Margins for a Supersonic Transport Configuration with a Variable-Sweep Wing
1967
18 pages
Report
Keine Angabe
Englisch
Aircraft , Air speed , Flight simulation , Pitch control , Supersonic transport , Variable sweep , Air , Altitude , Control , Flight , Maneuverability , Margin , Pitch , Simulation , Speed , Subsonic , Supersonic , Sweep , Transport , Variable , Wing
Variable sweep wing configuration Patent
NTRS | 1962
|Boeing variable-sweep supersonic transport
Engineering Index Backfile | 1965
|