Download
Download eBook for Free
| Format | File Size | Notes |
|---|---|---|
| PDF file | 3.5 MB | Use Adobe Acrobat Reader version 10 or higher for the best experience. |
Purchase
Purchase Print Copy
| Format | List Price | Price | |
|---|---|---|---|
| Add to Cart | Paperback111 pages | $30.00 | $24.00 20% Web Discount |
A study of aerodynamic design and performance of slender vehicles operating in high-altitude, high-velocity environments. The Memorandum: (1) briefly describes pertinent regimes of flight, and advances arguments to show that at high altitudes the leading-edge thickness is not dictated by convective and radiative heat-transfer rates; (2) describes flight regimes where leading-edge bluntness and hypersonic viscous interaction are important, and summarizes the theoretical approaches to these two limiting cases; (3) outlines a method of computing skin friction, heat transfer, and surface pressure in the viscous-interaction regime; (4) presents sample calculations which indicate that viscous interaction may significantly increase the lift and drag of slender vehicles.
Research conducted by
This report is part of the RAND Corporation Research memorandum series. The Research Memorandum was a product of the RAND Corporation from 1948 to 1973 that represented working papers meant to report current results of RAND research to appropriate audiences.
This document and trademark(s) contained herein are protected by law. This representation of RAND intellectual property is provided for noncommercial use only. Unauthorized posting of this publication online is prohibited; linking directly to this product page is encouraged. Permission is required from RAND to reproduce, or reuse in another form, any of its research documents for commercial purposes. For information on reprint and reuse permissions, please visit www.rand.org/pubs/permissions.
The RAND Corporation is a nonprofit institution that helps improve policy and decisionmaking through research and analysis. RAND's publications do not necessarily reflect the opinions of its research clients and sponsors.