Limitations of flight regime of a supersonic transport aircraft (SST) by sonic boom

被引：0
|
作者：
Kloster, M. [1 ]
机构：
[1] Lehrst. Flugmech. Flugregel., TU, Munchen, Germany
来源：
| 1976年 / 24卷 / 02期
关键词：
Compendex;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
AIRCRAFT
引用
收藏
页码：82 / 89
相关论文
共 50 条
  • [1] LIMITATIONS OF FLIGHT REGIME OF A SUPERSONIC TRANSPORT AIRCRAFT (SST) BY SONIC-BOOM
    KLOSTER, M
    ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1976, 24 (02): : 82 - 89
  • [2] LOW SONIC-BOOM SUPERSONIC TRANSPORT THROUGH AIRCRAFT DESIGN
    STUFF, R
    ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1976, 24 (01): : 34 - 38
  • [3] Reduction of the sonic boom level in supersonic aircraft flight by the method of surface cooling
    V. M. Fomin
    V. F. Chirkashenko
    V. F. Volkov
    A. M. Kharitonov
    Thermophysics and Aeromechanics, 2013, 20 : 669 - 678
  • [4] Reduction of the sonic boom level in supersonic aircraft flight by the method of surface cooling
    Fomin, V. M.
    Chirkashenko, V. F.
    Volkov, V. F.
    Kharitonov, A. M.
    THERMOPHYSICS AND AEROMECHANICS, 2013, 20 (06) : 669 - 678
  • [5] SONIC-BOOM RESEARCH AND DESIGN CONSIDERATIONS IN DEVELOPMENT OF A COMMERCIAL SUPERSONIC TRANSPORT (SST)
    HIGGINS, TH
    JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1965, 38 (05): : 914 - &
  • [6] Meteorologically induced variability of sonic-boom characteristics of supersonic aircraft in cruising flight
    Blumrich, R
    Coulouvrat, F
    Heimann, D
    JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 2005, 118 (02): : 707 - 722
  • [7] On sonic ray paths and sonic boom audiability zones generated by supersonic aircraft flight in temperature inhomogeneous atmosphere
    Svishchev, GP
    Khon'kin, AD
    DOKLADY AKADEMII NAUK, 1999, 369 (01) : 52 - 56
  • [8] SONIC BOOM AND SST
    THOMPSON, JR
    PARNELL, JE
    AIRCRAFT ENGINEERING, 1967, 39 (03): : 14 - &
  • [9] Wind effect on sonic ray paths and sonic boom audiability zones generated by supersonic aircraft flight in inhomogeneous atmosphere
    Svishchev, GP
    Khon'kin, AD
    DOKLADY AKADEMII NAUK, 1999, 369 (02) : 199 - 202
  • [10] An active control method for reducing sonic boom of supersonic aircraft
    Ye L.
    Ye Z.
    Ma B.
    Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2021, 39 (03): : 566 - 575
12345