d_mdo2007.flId = flightId
d_mdo2007.pid = \u9879\u76EEID
d_mdo2007.wid = \u6D41\u7A0Bid
d_mdo2007.tag = \u6807\u7B7E
d_mdo2007.reference_area = \u5168\u673A\u53C2\u8003\u9762\u79EF
d_mdo2007.max_zero_fuel = \u6700\u5927\u65E0\u71C3\u6CB9\u91CD\u91CF
d_mdo2007.max_takeoff = \u6700\u5927\u8D77\u98DE\u91CD\u91CF
d_mdo2007.max_landing = \u6700\u5927\u7740\u9646\u91CD\u91CF
d_mdo2007.c_x = \u91CD\u5FC3\u4F4D\u7F6Ex
d_mdo2007.c_y = \u91CD\u5FC3\u4F4D\u7F6Ey
d_mdo2007.c_z = \u91CD\u5FC3\u4F4D\u7F6Ez
d_mdo2007.mw_n_sections = \u673A\u7FFC\u673A\u7FFC\u6BB5\u6570
d_mdo2007.mw_span = \u673A\u7FFC\u7FFC\u5C55
d_mdo2007.mw_mac = \u673A\u7FFC\u5E73\u5747\u6C14\u52A8\u5F26\u957F
d_mdo2007.mw_sweep = \u673A\u7FFC\u540E\u63A0\u89D2
d_mdo2007.mw_aspect_ratio = \u673A\u7FFC\u5C55\u5F26\u6BD4
d_mdo2007.mw_area = \u673A\u7FFC\u673A\u7FFC\u9762\u79EF
d_mdo2007.mw_thickness_to_chord = \u673A\u7FFC\u539A\u5F26\u6BD4
d_mdo2007.mwf_span_fraction_start = \u895F\u7FFC\u5C55\u5411\u8D77\u59CB\u4F4D\u7F6E
d_mdo2007.mwf_span_fraction_end = \u895F\u7FFC\u5C55\u5411\u7EC8\u6B62\u4F4D\u7F6E
d_mdo2007.mwf_deflection = \u895F\u7FFC\u504F\u89D2
d_mdo2007.mwf_chord_fraction = \u895F\u7FFC\u5F26\u5411\u5360\u6BD4
d_mdo2007.mwf_configuration_type = \u895F\u7FFC\u7C7B\u578B
d_mdo2007.mwa_span_fraction_start = \u526F\u7FFC\u5C55\u5411\u8D77\u59CB\u4F4D\u7F6E
d_mdo2007.mwa_span_fraction_end = \u526F\u7FFC\u5C55\u5411\u7EC8\u6B62\u4F4D\u7F6E
d_mdo2007.mwa_deflection = \u526F\u7FFC\u504F\u89D2
d_mdo2007.mwa_chord_fraction = \u526F\u7FFC\u5F26\u5411\u5360\u6BD4
d_mdo2007.hw_n_sections = \u5347\u964D\u8235\u5E73\u5C3E\u6BB5\u6570
d_mdo2007.hw_span = \u5347\u964D\u8235\u7FFC\u5C55
d_mdo2007.hw_mac = \u5347\u964D\u8235\u5E73\u5747\u6C14\u52A8\u5F26\u957F
d_mdo2007.hw_sweep = \u5347\u964D\u8235\u540E\u63A0\u89D2
d_mdo2007.hw_aspect_ratio = \u5347\u964D\u8235\u5C55\u5F26\u6BD4
d_mdo2007.hw_area = \u5347\u964D\u8235\u673A\u7FFC\u9762\u79EF
d_mdo2007.hw_thickness_to_chord = \u5347\u964D\u8235\u539A\u5F26\u6BD4
d_mdo2007.hwe_span_fraction_start = \u5347\u964D\u8235\u5C55\u5411\u8D77\u59CB\u4F4D\u7F6E
d_mdo2007.hwe_span_fraction_end = \u5347\u964D\u8235\u5C55\u5411\u7EC8\u6B62\u4F4D\u7F6E
d_mdo2007.hwe_deflection = \u5347\u964D\u8235\u504F\u89D2
d_mdo2007.hwe_chord_fraction = \u5347\u964D\u8235\u5F26\u5411\u5360\u6BD4
d_mdo2007.vw_n_sections = \u5782\u5C3E\u6BB5\u6570
d_mdo2007.vw_span = \u5782\u5C3E\u7FFC\u5C55
d_mdo2007.vw_mac = \u5782\u5C3E\u5E73\u5747\u6C14\u52A8\u5F26\u957F
d_mdo2007.vw_sweep = \u5782\u5C3E\u540E\u63A0\u89D2
d_mdo2007.vw_aspect_ratio = \u5782\u5C3E\u5C55\u5F26\u6BD4
d_mdo2007.vw_area = \u5782\u5C3E\u673A\u7FFC\u9762\u79EF
d_mdo2007.vw_thickness_to_chord = \u5782\u5C3E\u539A\u5F26\u6BD4
d_mdo2007.f_length = \u673A\u8EAB\u603B\u957F
d_mdo2007.f_diameter = \u673A\u8EAB\u5BBD\u5EA6
d_mdo2007.n_symmetry = \u673A\u8231\u662F\u5426\u5BF9\u79F00\u4E0D\u5BF9\u79F01\u5BF9\u79F0
d_mdo2007.n_length = \u673A\u8231\u957F\u5EA6
d_mdo2007.n_diameter = \u673A\u8231\u76F4\u5F84
d_mdo2007.n_x = \u673A\u8231\u539F\u70B9\u4F4D\u7F6Ex
d_mdo2007.n_y = \u673A\u8231\u539F\u70B9\u4F4D\u7F6Ey
d_mdo2007.n_z = \u673A\u8231\u539F\u70B9\u4F4D\u7F6Ez
d_mdo2007.network_tag = \u52A8\u529B\u7F51\u7EDC\u6807\u7B7E
d_mdo2007.fuel_consumption_rate = \u52A8\u529B\u7F51\u7EDC\u71C3\u6CB9\u6D88\u8017\u7387
d_mdo2007.num_of_engines = \u52A8\u529B\u7F51\u7EDC\u53D1\u52A8\u673A\u4E2A\u6570
d_mdo2007.engine_length = \u52A8\u529B\u7F51\u7EDC\u53D1\u52A8\u673A\u957F\u5EA6
d_mdo2007.engine_diameter = \u52A8\u529B\u7F51\u7EDC\u53D1\u52A8\u673A\u76F4\u5F84
d_mdo2007.bypass_ratio = \u52A8\u529B\u7F51\u7EDC\u6DB5\u9053\u6BD4
d_mdo2007.design_thrust = \u52A8\u529B\u7F51\u7EDC\u8BBE\u8BA1\u63A8\u529B
d_mdo2007.takeoff_flap_deflection = \u8D77\u98DE\u8BBE\u7F6E\u895F\u7FFC\u504F\u89D2
d_mdo2007.takeoff_v2_vs_ratio = \u8D77\u98DE\u8BBE\u7F6EV2\u901F\u5EA6\u6216\u5931\u901F\u901F\u5EA6
d_mdo2007.landing_flap_deflection = \u7740\u9646\u8BBE\u7F6E\u895F\u7FFC\u504F\u89D2
d_mdo2007.landing_slat_deflection = \u7740\u9646\u8BBE\u7F6E\u7F1D\u7FFC\u504F\u89D2
d_mdo2007.landing_vref_vs_ratio = \u7740\u9646\u8BBE\u7F6E\u8FDB\u573A\u901F\u5EA6\u6216\u5931\u901F\u901F\u5EA6
d_mdo2007.airport_tag = \u673A\u573A\u6807\u7B7E
d_mdo2007.airport_altitude = \u673A\u573A\u6D77\u62D4\u9AD8\u5EA6
d_mdo2007.airport_delta_isa = \u673A\u573AISA\u504F\u5DEE
d_mdo2007.cruise_altitude = \u5DE1\u822A\u9AD8\u5EA6
d_mdo2007.cruise_mach = \u5DE1\u822A\u9A6C\u8D6B\u6570
d_mdo2007.envelope_machs = \u98DE\u884C\u5305\u7EBF\u9A6C\u8D6B\u6570
d_mdo2007.envelope_altitudes = \u98DE\u884C\u5305\u7EBF\u9AD8\u5EA6
d_mdo2007.stability_mach = \u7A33\u5B9A\u6027\u8BA1\u7B97\u8F93\u5165\u9A6C\u8D6B\u6570
d_mdo2007.stability_altitude = \u7A33\u5B9A\u6027\u8BA1\u7B97\u8F93\u5165\u6D77\u62D4\u9AD8\u5EA6
d_mdo2007.minimal_flight_speed = \u6700\u5C0F\u5E73\u98DE\u901F\u5EA6
d_mdo2007.maximal_flight_speed = \u6700\u5927\u5E73\u98DE\u901F\u5EA6
d_mdo2007.rate_of_climb = \u722C\u5347\u7387
d_mdo2007.ceiling = \u5347\u9650
d_mdo2007.range = \u822A\u7A0B
d_mdo2007.time = \u822A\u65F6
d_mdo2007.takeoff_field_length = \u8D77\u98DE\u573A\u957F
d_mdo2007.landing_field_length = \u7740\u9646\u573A\u957F
d_mdo2007.cm_alpha = \u7EB5\u5411\u9759\u7A33\u5B9A\u5BFC\u6570
d_mdo2007.cn_beta = \u822A\u5411\u9759\u7A33\u5B9A\u5BFC\u6570
d_mdo2007.phugoid_zeta = \u957F\u5468\u671F\u6A21\u6001\uFF08\u963B\u5C3C\u6BD4\uFF09
d_mdo2007.phugoid_omega_n = \u957F\u5468\u671F\u6A21\u6001\uFF08\u9891\u7387\uFF09
d_mdo2007.short_period_zeta = \u77ED\u5468\u671F\u6A21\u6001\uFF08\u963B\u5C3C\u6BD4\uFF09
d_mdo2007.short_period_omega_n = \u77ED\u5468\u671F\u6A21\u6001\uFF08\u9891\u7387\uFF09
d_mdo2007.spiral_tau = \u87BA\u65CB\u6A21\u6001\uFF08\u65F6\u95F4\u5E38\u6570\uFF09
d_mdo2007.roll_tau = \u6EDA\u8F6C\u6A21\u6001\uFF08\u65F6\u95F4\u5E38\u6570\uFF09
d_mdo2007.dutch_roll_zeta = \u8377\u5170\u6EDA\u6A21\u6001\uFF08\u963B\u5C3C\u6BD4\uFF09
d_mdo2007.dutch_roll_omega_n = \u8377\u5170\u6EDA\u6A21\u6001\uFF08\u9891\u7387\uFF09
d_mdo2007Form = true