Some Aerodynamic and Control Studies of Lifting Reentry Configurations at Angles of Attack Up to 90 Deg at a Mach Number Of 2.91
Overview & Synopsis
Aerodynamic and control studies of lifting reentry configurations at angles of attack up to 90-deg at supersonic speeds
Indexed from repository: NASA Technical Reports Server
(
ntrs.nasa.gov)
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Document Information
| Document Title | Some Aerodynamic and Control Studies of Lifting Reentry Configurations at Angles of Attack Up to 90 Deg at a Mach Number Of 2.91 |
|---|---|
| Author / Organization | Clark, F. L., Evans, J. 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-68942 |
| Original Source Link | Visit Source Page on ntrs.nasa.gov » |