PROPULSION SYSTEM INTEGRATION AS APPLIED TO BUSINESS JET AIRCRAFT

被引：0
|
作者：
SUGGS, JP [1 ]
BURLEY, GW [1 ]
机构：
[1] GARRETT TURBINE ENGINE CO,PHOENIX,AZ
来源：
MECHANICAL ENGINEERING | 1983年 / 105卷 / 06期
关键词：
D O I：
暂无
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
引用
收藏
页码：92 / 92
页数：1
相关论文
共 50 条
  • [31] Investigations of propulsion integration interference effects on a transport aircraft configuration
    Rossow, C.-C.
    Godard, J.-L.
    Hoheisel, H.
    Schmitt, V.
    1600, AIAA, Washington, DC, United States (31):
  • [32] HTS Electrical System for a Distributed Propulsion Aircraft
    Berg, Frederick
    Palmer, Joseph
    Miller, Paul
    Husband, Mark
    Dodds, Graham
    IEEE TRANSACTIONS ON APPLIED SUPERCONDUCTIVITY, 2015, 25 (03)
  • [33] NOISE EMISSION FROM AIRCRAFT PROPULSION SYSTEM
    KISTLER, AL
    MECHANICAL ENGINEERING, 1972, 94 (05) : 62 - &
  • [34] Simulation Model of a Propulsion System of a Supersonic Aircraft
    Alendar’ A.D.
    Siluyanova M.V.
    Russian Engineering Research, 2021, 41 (07) : 676 - 679
  • [35] Raytheon Aircraft unveils Hawker Horizon business jet
    Anon
    2001, McGraw-Hill Companies Inc. (154):
  • [36] Raytheon Aircraft unveils Hawker Horizon business jet
    Phillips, EH
    AVIATION WEEK & SPACE TECHNOLOGY, 2001, 154 (17): : 48 - 48
  • [37] Propulsion system integration on truss-braced aircraft: structural performance sensitivity to architectural design parameters
    Quinn, Damian
    Colbert, Stephen
    Nolan, Declan C.
    Fox, Rob
    Gaskell, Jill
    AEROSPACE SCIENCE AND TECHNOLOGY, 2025, 159
  • [38] Uncertainty quantification and robust design optimization applied to aircraft propulsion systems
    Panzeri, Marco
    Savelyev, Andrey
    Anisimov, Kirill
    d'Ippolito, Roberto
    Mirzoyan, Artur
    AEROSPACE EUROPE CEAS 2017 CONFERENCE, 2018, 29 : 289 - 302
  • [39] THE JET PROPULSION LABORATORY EPHEMERIS TAPE SYSTEM
    OROZCO, EG
    COMMUNICATIONS OF THE ACM, 1964, 7 (10) : 568 - 568
  • [40] PRESSURE-JET HELICOPTER PROPULSION SYSTEM
    NICHOLS, JB
    AERONAUTICAL JOURNAL, 1972, 76 (741): : 552 - &
12345