Takeoff is numerically investigated in non-dimensional terms assuming constant takeoff speed; simple analysis of climbing after takeoff can be made up to obstacle clearance height; takeoff distances indicate possibilities resulting from using aircraft designed for vertical, short takeoff runs, over range of thrust extending from S0/G-0.8 to 1.0.
Calculation of takeoff run of aircraft with engine-thrust tilting
Zur Berechnung der Kurzstartleistungen von Flugzeugen mit Schubschwenk-Triebwerken
Zeitschrift fuer Flugwissenschaften ; 8 , n 3
1960
7 pages
Aufsatz (Zeitschrift)
Deutsch
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