Subsonic/transonic free-flight tests of a generic missile with grid fins-Reference-Cited by-同舟云学术

Subsonic/transonic free-flight tests of a generic missile with grid fins

Published:2000-01-10 Issue: Volume: Page:
ISSN:
Container-title:38th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Abate Gregg¹,Duckerschein Ralf¹,Hathaway Wayne²

Affiliation:

1. USAF, Research Lab., Eglin AFB, FL

2. ArrowTech Associates, South Burlington, VT

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-937

Reference20 articles.

1. (kg/m^3) xCCL Mach c .1-o f CNu c ma c "I`, x <`./L 1.2012 0.574 0.695 7.630 I.2030 0.744 0.77 1 7.620 1.1974 0.771 0.812 4.860 I .2030 0.817 0.831 7.390 I.1967 0.879 0.883 7.700 1.2078 0.905 0.969 7.910 I .2019 1.045 I.013 8.490 I.2005 I.135 I.008 8.170 I.1971 I.146 I.030 7.260 I.I969 1.190 0.949 6.970 I.1955 1.332 0.963 6.760 1.1969 1.521 0.926 5.970 I.1966 I.590 0.928 6.580

2. 757 0.192 4.520 0.841 0.935 7.660 0.867 0.901 7.660 I.129 I.021 8.170 I.411 0.939 6.090 -I 7.994 -6.997 -2 I.594 -24.094 -24.134 -28.067 -24.158 -25.920 -22.438 -19.647 -9.409 -8.868

3. 35 I -23.024 -22.486 -25.625 -10.799 1.2020 0.388 0.344 I.2008 0.580 0.336 9.210 1.2043 0.638 0.343 IO.020 I.2221 O.YO8 0.415 14.780

4. 535 0.341 9.860 -36.494 -41.530 -39.356 -56.403 -39.675 -415.2

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