Two simplified versions of supersonic area rule

被引:1
作者
Nikolic, VR [1 ]
Jumper, EJ
机构
[1] Minnesota State Univ, Dept Mech Engn, Mankato, MN 56001 USA
[2] Univ Notre Dame, Dept Aerosp & Mech Engn, Notre Dame, IN 46556 USA
来源
JOURNAL OF AIRCRAFT | 2005年 / 42卷 / 02期
关键词
D O I
10.2514/1.7149
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The simplified versions of the Jones formula, known as the supersonic area rule, which includes Jumper's simplification and four new proposed simplifications, are described. The Jones formula has been a major tool in the design and analysis of supersonic aircraft since its introduction. The Jumper simplification has been the first major modification of the standard supersonic area rule. Four new methods were developed, one of which provided interesting rules. The method uses cuts with the downstream Mach cone lateral surface on the equivalent body of revolution. The Jumper method proved superior to the new simplification at transonic and lower supersonic speeds.
引用
收藏
页码:551 / 555
页数:5
相关论文
共 14 条
  • [1] BAALS DD, 1970, J AIRCRAFT, V7, P385
  • [2] Harris R., 1964, X947 NASA TM
  • [3] JONES RT, 1956, 1284 NACA
  • [4] WAVE DRAG PREDICTION USING A SIMPLIFIED SUPERSONIC AREA RULE
    JUMPER, EJ
    [J]. JOURNAL OF AIRCRAFT, 1983, 20 (10): : 893 - 895
  • [5] LEMLEY CE, 1978, AFWALTR803058 FLIGHT
  • [6] LIEPMAN HW, 2002, ELEMENT GAS DYNAMICS, P235
  • [7] LUOMA AA, 1957, SL57H06 NASA RM
  • [8] LUOMA AA, 1956, SL56D12 NASA RM
  • [9] MEYER WL, 1976, 4589 MDC
  • [10] Nikolic V., 2004, 2004217 AIAA