EASA Certification Information 2010-01
12 févr. 2010 BAC 1-11 aircraft registered in an EU Member State will no longer be eligible for a Normal Certificate of Airworthiness in accordance with ...
Untitled
SA-393. AIRCRAFT ACCIDENT REPORT. Adopted: April 18 1968. BRANIFF AIRWAYS
BAC 1-11 Fueling Procedures Introduction The Bac 1-11 Model 200
Secure fuel panel and disconnect from aircraft. Alternate Refueling Procedures. The following procedure may be used for fueling should the load control or fuel
Application Story «
BAC 1-11 trials aircraft acting as a „surrogate“ unmanned air vehicle (UAV). the BAC 1-11 acting as a surrogate UAV and three simulated UAVs.
Page No. 1 2 3 4 5 6 7 8 9 10 Rev. No. 28 28 28 28 28 28 28 28 28
31 août 2011 I. BAC 1-11 200 Series (Transport Aircraft) Approved April 15 1965 for Model/Type 203/AE. Amended May 13
Air Accidents I nvest ig at i on Branch
10 juin 1990 AIRCRAFT ACCIDENT REPORT 1/92. Air Accidents Investigation Branch. Department of Transport. Report on the accident to. BAC One-Eleven G-B ...
Deep stall characterization and identification algorithm on a T-tail
3 avr. 2015 first observed during a BAC 1-11 test-flight leading to crash. The flight of the tail inside the separated wake of the stalled main wing ...
Untitled
AIRCRAFT ACCIDENT REPORT. MOHAWK AIRLINES. INC. BAC 1-11
Untitled
Accidents Investigation Branch. Aircraft Accident Report No. 7/78. (EW/C615). Operator: Monarch Airways Ltd. Aircraft: Type: BAC 1-11.
2MiB}+ `2b2`+? /Q+mK2Mib- r?2i?2` i?2v `2 Tm#@
HBb?2/ Q` MQiX h?2 /Q+mK2Mib Kv +QK2 7`QK
i2+?BM; M/ `2b2`+? BMbiBimiBQMb BM 6`M+2 Q` #`Q/- Q` 7`QK Tm#HB+ Q` T`Bpi2 `2b2`+? +2Mi2`bX /2biBMû2 m /ûT¬i 2i ¨ H /BzmbBQM /2 /Q+mK2Mib b+B2MiB}[m2b /2 MBp2m `2+?2`+?2- Tm#HBûb Qm MQM-Tm#HB+b Qm T`BpûbX
.22T biHH +?`+i2`BxiBQM M/ B/2MiB}+iBQM H;Q`Bi?KQM h@iBH B`+`7i KQ/2H
Gm`2Mi >2i`m- h?B2``v JX 6m`2- a2#biB2M EQH#- PHBpB2` JQMi;MB2` hQ +Bi2 i?Bb p2`bBQM, Gm`2Mi >2i`m- h?B2``v JX 6m`2- a2#biB2M EQH#- PHBpB2` JQMi;MB2`X .22T biHH +?`+i2`BxiBQM M/ B/2MiB}+iBQM H;Q`Bi?K QM h@iBH B`+`7i KQ/2HX 8yi? j6 AMi2`MiBQMH *QM72`2M+2 QM TTHB2/2`Q/vMKB+b- bbQ+BiBQM û`QMmiB[m2 2i bi`QMmiB[m2 /2 6`M+2 @ j6- J` kyR8- hQmHQmb2-
6`M+2X e TX ?H@yRRj3Nje
50th 3AF International Conference on
Applied Aerodynamics
Toulouse, France, 30-31 March, 1 April, 2015
FPDeep stall characterizati
Laurent Hetru ,
, , Olivier Montagnier (1) Air Force Research Center (CReA)Email:
olivier.m (2) nieur, (ceABSTRACT
The I q,INTRODUCTION
e x CmD, Wc q WS T AOA1.GENERA
q, e q, MODE X U e x `^`xUGJD,Figure 1. Pitching aerodynamic coefficients for
The a
eCD, eCD, eCmD, qCm qCm q q2 DGDGDFigure 2.
q3.TYPICAL PHASE PORTRAIT
e 0 eqD0wwDCm
0D 0q 0D 0q - Figure 3 q,4.SHORT PER
q q, spm spm e mV q UUZ[ UUZ D D cos m yI, y coeffi LC qCm deg e s/ 1.52i 04spm 52spms/ 1.76i 37spm
89spm