| Title | Journal | Journal Categories | Citations | Publication Date |
|---|---|---|---|---|
| Eleventh Annual Meeting, I.Ae.S. | 1943 | |||
| t h e m a x i m u m | ||||
| indicated= n P - r e q d . (°V ) | ||||
| I n Fig. 14 this ratio is computed for conditions of cruising speed (as previously defined) because it is under | ||||
| I n Fig. 12 this ratio is computed under conditions of flight for best range (as previously defined). I t is under the conditions of best range t h a t the pay-load factor attains t h e higher value |