 Balancing loads. Loads by which the airplane is placed in a state of equilibrium under the action of external forces resulting from specified loading conditions. The state of equilibrium thus obtained may be either real or fictitious. Balancing loads...  Basic Glider Criteria Handbook - Էջ xvUnited States. Flight Standards Service - 1962 - 139 էջԱմբողջությամբ դիտվող - Այս գրքի մասին
 | 1939 - 1220 էջ
...period of at least one minute. (See § 04.201.) 04.128 Balancing loads. Loads by which the airplane is placed in a state of equilibrium under the action...loads may represent air loads, inertia loads, or both. (See § 04.2210.) 04.129 Aerodynamic coefficients, CL, CM, CP, etc. The coefficients hereinafter specified... | |
 | 1961 - 1484 էջ
...for a period of at least 1 minute. (See §4a.62.) (j) Balancing loads. Loads by which the airplane is placed in a state of equilibrium under the action...loads may represent air loads, inertia loads, or both. (See § 4a.ll6.) § 4a.44 Aerodynamic coefficients, CL, CM, CP, etc. The coefficients hereinafter specified... | |
 | 1962 - 898 էջ
...for a period of at least 1 minute. (See i 4a.62.) (j) Balancing loads. Loads by which the airplane is placed in a state of equilibrium under the action...loads may represent air loads, inertia loads, or both. (See i 411.116. > § 4a.44 Aerodynamic coefficient*, Cj,, CM, CP, etc. The coefficients hereinafter... | |
 | 1962 - 966 էջ
...for a period of at least 1 minute. (See §4a.62.) ( j ) Balancing loads. Loads by which the airplane is placed in a state of equilibrium under the action...loads may represent air loads, inertia loads, or both. (See § 4a.ll6.) § la. 1 1 Aerodynamic coefficients, CL, CM, CP, etc. The coefficients hereinafter... | |
 | 1961 - 1480 էջ
...for a period of at least 1 minute. (See §4a.62.) (j) Balancing loads. Loads by which the airplane is placed in a state of equilibrium under the action...loads may represent air loads, inertia loads, or both. (See § 4a.ll6.) § 4a.44 Aerodynamic coefficients, CL, CM, CP, etc. The coefficients hereinafter specified... | |
 | 1949 - 582 էջ
...for a period of at least 1 minute. (See § 4a.62.) (j) Balancing loads. Loads by which the airplane is placed in a state of equilibrium under the action...loads may represent air loads, inertia loads, or both. (See § 4a.ll6.) § 4a.44 Aerodynamic coefficients, CL, CM, CP, etc. The coefficients hereinafter specified... | |
 | 1952 - 1006 էջ
...for a period of at least 1 minute. (See § 4a.62.) <j) Balancing loads. Loads by which the airplane is placed in a state of equilibrium under the action...loads may represent air loads, inertia loads, or both. (See § 4a.ll6.) § 4a.44 Aerodynamic coefficients, CL, Ca, CP, etc. The coefficients hereinafter specified... | |
 | 1964 - 924 էջ
...for a period of at least 1 minute. (See §4a.62.) (j) Balancing loads. Loads by which the airplane is placed in a state of equilibrium under the action...loads may represent air loads, inertia loads, or both. (See § 4a.ll6.) § •In. 1 1 Aerodynamic coefficients, CL, CM, CP, etr. The coefficients hereinafter... | |
 | 1963 - 920 էջ
...for a period of at least 1 minute. (See § 4a.62.) (J) Balancing loads. Loads by which the airplane is placed in a state of equilibrium under the action...loads may represent air loads, inertia loads, or both. (See !4a.ll6.) § 4a.44 Aerodynamic coefficient*, CL, CM, CP, etc. The coefficients hereinafter specified... | |
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