A Wind-tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 at Angles of Attack to 90 Deg
Overview & Synopsis
High angle aerodynamic characteristics produced by nose cone of revolution in wind tunnel at supersonic speed
Indexed from repository: NASA Technical Reports Server
(
ntrs.nasa.gov)
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Document Information
| Document Title | A Wind-tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 at Angles of Attack to 90 Deg |
|---|---|
| Author / Organization | Smith, F. M. |
| Subject & Discipline | TECHNICAL_MEMORANDUM |
| Categories | Aerospace & Aviation |
| Publication Year | 2019 |
| License / Rights | Public Domain / NASA STI Open Access |
| Resource Verification | Listed PDF (Verification Pending) |
| Original Host Website |
NASA Technical Reports Server
(ntrs.nasa.gov)
|
| File Format | application/pdf (Portable Document Format) |
| Language | EN |
| Catalog ID | DOC-82622 |
| Original Source Link | Visit Source Page on ntrs.nasa.gov » |