 | 1963 - 920 էջ
...required in i 4a.99. § 4a.45 Standard atmosphere (standard air). Standard atmosphere refers to that variation of air conditions with altitude which has...safety of the airplane. [Amdt. 5, 4 FR 1171, Mar. 9, 1939] Subpart C — Structural Loading Conditions SOURCE: 5l4a.61 to 4a.216 contained In Civil Air... | |
 | 1961 - 1480 էջ
...required in f 4a.99. § 4a. 15 Standard atmosphere (standard air). Standard atmosphere refers to that variation of air conditions with altitude which has...seriously endanger the safety of the airplane. [Amdt. 6, 4 FB 1171, Mar. 9, 1939] SubpartC — Structural Loading Conditions SOURCE: §§ 4a.61 to 4a.21G... | |
 | 1964 - 924 էջ
...required in § 4a.99. § 4a.45 Standard atmosphere (standard air). Standard atmosphere refers to that variation of air conditions with altitude which has...would seriously endanger the safety of the airplane. lAiuclt. 5. 4 FB 1171. Mar. 9. 1939] Subpart C — Structural Loading Conditions SOURCE: i!4a.61 to... | |
 | United States. Department of State - 1940 - 806 էջ
...deflected Vl critical engine failure speed V, minimum take-off-climb speed 2.024. Structural Terms. Primary Structure. Those portions of the airplane...would seriously endanger the safety of the airplane. Design Wing Area, S. The area enclosed by the wing outline (including ailerons, and flaps in the retracted... | |
 | 1949 - 582 էջ
...required in § 4a.99. § 4a.45 Standard atmosphere (standard air). Standard atmosphere refers to that variation of air conditions with altitude which has...adopted as standard in the United States. (See any aeronautics text book or handbook, or NACA Technical Report No. 218.) I 4a.46 Primary structure. Those... | |
 | 1952 - 1006 էջ
...required in § 4a.99. § 4a.45 Standard atmosphere (standard air). Standard atmosphere refers to that variation of air conditions with altitude which has...adopted as standard in the United States. (See any aeronautics text book or handbook, or NACA Technical Report No. 218.) § 4a.46 Primary structure. Those... | |
| |
... subscripts have the usual significance. When applied to an entire wing or surface, the coefficients represent average values and shall be properly correlated with local conditions (load distribution) as required in i 4a.99. 
