《A SHOCK TUBE INVESTIGATION OF SILO-LAUNCHED VEHICLE AERODYNAMIC FLOW ASYMMETRIES》
| 作者 | 编者 |
|---|---|
| 出版 | 未查询到或未知 |
| 参考页数 | 63 |
| 出版时间 | 没有确切时间的资料 |
| ISBN号 | 无 — 求助条款 |
| PDF编号 | 811808238（仅供预览，未存储实际文件） |
| 求助格式 | 扫描PDF（若分多册发行，每次仅能受理1册） |
《A SHOCK TUBE INVESTIGATION OF SILO-LAUNCHED VEHICLE AERODYNAMIC FLOW ASYMMETRIES》由于是年代较久的资料都绝版了，几乎不可能购买到实物。如果大家为了学习确实需要，可向博主求助其电子版PDF文件。对合法合规的求助，我会当即受理并将下载地址发送给你。
高度相关资料
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- AN EXPLORATORY INVESTIGATION OF THE EFFECTS OF IONIZATION ON THE FLOW AND HEAT TRANSFER WITH A DENSE
- 1963 DEPARTMENT OF COMMERCE
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- FUNDAMENTAL DATA OBTAINED FROM SHOCK-TUBE EXPERIMENTS
- 1961 PERGAMON PRESS
-
- A GEOMETRIC INVESTIGATION OF REACH
- THE MIT PRESS
-
- AERODYNAMIC STUDIES:The Forces Acting On An Air Vehicle A Review of the Literature
- WRIGHT AIR DEVELOPMENT CENTER
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- EXPERIMENTAL INVESTIGATION OF INFLUENCE OF EDGE SHAPE ON THE AERODYNAMIC CHARACTERISTICS OF LOW-ASPE
- Cornell Aeronautical Laboratory
-
- A SHOCK-TUBE INVESTIGATION OF DETONATIVE COMBUSTION
- 1955 ENGINEERING RESEARCH INSTITUTE UNIVERSITY OF MICHIGAN
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