Estimating Rebound Effects for International Air Routes in Korea: Using Airlines’ Flight Performance Data on Four Europe Routes

2021 ◽  
Vol 23 (2) ◽  
pp. 95-123
Author(s):  
Sang-Yong Han
Keyword(s):  
Performance Data ◽  
Flight Performance ◽  
Rebound Effects

scholarly journals Archeops in-flight performance, data processing, and map making

2007 ◽  
Vol 467 (3) ◽  
pp. 1313-1344 ◽  
Author(s):  
J. F. Macías-Pérez ◽  
G. Lagache ◽  
B. Maffei ◽  
K. Ganga ◽  
A. Bourrachot ◽  
...  
Keyword(s):  
Data Processing ◽  
Performance Data ◽  
Flight Performance

Design of Flight Performance Calculation Component for UAV Mission Planning Based on Performance Data Package

2021 ◽  
pp. 994-1002
Author(s):  
Huan Xie ◽  
Yiheng Pan ◽  
Rui Li ◽  
Chuyun Huang ◽  
Linmin Yan ◽  
...  
Keyword(s):  
Performance Data ◽  
Mission Planning ◽  
Flight Performance ◽  
Performance Calculation

Orbiting Astronomical Observatory heat pipe flight performance data

1973 ◽  
Author(s):  
W. HARWELL ◽  
F. EDELSTEIN ◽  
R. MCINTOSH ◽  
S. OLLENDORF
Keyword(s):  
Heat Pipe ◽  
Astronomical Observatory ◽  
Performance Data ◽  
Flight Performance

Effects of Chemical Defense Antidotes (Atropine) on Aviator Performance (Simulated Flight and Zero Input Tracking Analyzer)

1986 ◽  
Vol 30 (12) ◽  
pp. 1187-1191
Author(s):  
Lewis W. Stone ◽  
Ronald R. Simmons ◽  
Heber D. Jones ◽  
David J. Carter ◽  
Roger S. Christiansen
Keyword(s):  
Chemical Defense ◽  
Saline Solution ◽  
Atropine Sulfate ◽  
Performance Data ◽  
Biological Warfare ◽  
Chemical Agent ◽  
Flight Performance ◽  
Paper Briefly ◽  
Psychomotor Effects ◽  
Systematic Program

Army aviation is at serious risk in chemical and biological warfare environments. One of the potential countermeasures for aviators against the chemical threat is the development of antidote and pretreatment drugs. Just as the chemical agent carries the threat of degrading aviator performance, antidote and pretreatment drugs could independently produce problems either alone or in combination with an agent. This paper briefly outlines part of the first phase of a systematic program using controlled, simulated flight conditions and a Zero Input Tracking Analyzer (ZITA) to identify and measure flight performance and psychomotor effects of unchallenged atropine (one of the chemical defense antidotes) on aviators. Each of 12 U.S. Army helicopter aviators voluntarily received 3 dosages: 0 mg (saline solution), 2 mg of atropine sulfate, and 4 mg of atropine sulfate. Results indicate that simulator flight performance data did prove to be sensitive in identifying and measuring effects of 4 mg of atropine. Additionally, some ZITA tests showed a statistically significant degradation with the 4 mg dosage.

scholarly journals Metoda Short Takeoff Landing (Studi Kasus Prestasi Terbang Takeoff-Landing Pesawat Udara Turbo Prop CN235)

WARTA ARDHIA ◽  
2017 ◽  
Vol 41 (2) ◽  
pp. 49
Author(s):  
Sayuti Syamsuar
Keyword(s):  
Critical Condition ◽  
Aerospace Industry ◽  
Aerodynamic Performance ◽  
Performance Data ◽  
Flight Performance ◽  
Aircraft Structure ◽  
Trade Off ◽  
Study Case ◽  
Full Throttle ◽  
Obstacle Height

The aircraft category of Short Take-Off Landing, in general, including lightweight aircrafts with take-off weight between 20.000 lb (9.072 kg) and 50.000 lb (22.680 kg) and capable in exceeding 50 ft (15 m) obstacle height with only 1.500 ft (450 m) of take-off and landing distance. Thera are, at least, three general requirements that have to be considered in order to develop this category of aircraft; high aerodynamic performance, powerful engine, qualified skill of pilot, and also the strength of aircraft structure that can sustain heavy load.As for the study case, the author used the flight performance data of CN235-100 (serial N-16) Short Field Landing with 230 flap that was tested in Indonesian Aerospace Industry in 1996 for its trade-off performance. There was also rejected take-off or accelerate stop distance test with 100 flap and full throttle where one of the engine, then suddenly, shut down in order to achieve critical condition and later the power of the another engine being reduced by the pilot so that the aircraft can stop at the end of the runway. Several pilot recommendations are given in the conclusion chapter. Keywords: short take-off landing, height, distance, performance, engine, pilot, flap. Pesawat dengan kategori Short Take-Off Landing pada umumnya adalah pesawat ringan yang mempunyai berat take-off antara 20.000 lb (9.072 kg) hingga 50.000 lb (22.680 kg) dengan kemampuan melewat irintangan setinggi 50 ft (15 m) untuk jarak take-off dan landing sejauh 1.500 ft (450 m). Pengembangan pesawat dengan kategori tersebut perlu memperhatikan tiga persyaratan umum yaitu kemampuan aerodinamika yang tinggi, tenaga mesin yang besar, dan teknik pilot yang baik yang disertai dengan kekuatan struktur yang mampu menahan beban berat. Pada studi kasus ini, penulis menggunakan data prestasi terbang Short Field Landing pesawat CN235-100 (serial N-16) dengan menggunakan flap 230 pada saat pengujian performance trade-off di PT Dirgantara Indonesia pada tahun 1996. Pengujian tersebut juga termasuk uji rejected take-off atau accelerate stop distance dengan menggunakan flap 100 pada tenaga penuh dimana kemudian salah satu mesin dimatikan untuk mencapai kondisi kritis dan pilot mengurangi daya propulsi mesin lainnya untuk dapat berhenti di ujung landasan. Beberapa rekomendasi pilot diberikan pada bagian kesimpulan. Kata kunci: short takeoff landing, tinggi, jarak, performance, engine, pilot, flap.

Real-Time Performance Data Improved VTE Prophylaxis

2009 ◽  
Vol 2 (6) ◽  
pp. 4
Author(s):  
PATRICE WENDLING
Keyword(s):  
Real Time ◽  
Performance Data ◽  
Vte Prophylaxis ◽  
Time Performance

ATTRITION DATA AS A CRITERION: I. REASONS FOR WITHDRAWAL AND FLIGHT PERFORMANCE.

1954 ◽  
Author(s):  
Wilse B. Webb ◽  
John T. Bair ◽  
Rosalie K. Ambler
Keyword(s):  
Flight Performance
Sign in / Sign up

Export Citation Format

Share Document