Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 / Jim A. Penland, James B. Hallissy, and James L. Dillon.
| Author/creator | Penland, Jim A. author. |
| Format | Electronic |
| Publication | Washington, District of Columbia : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1979. |
| Description | 1 online resource (144 pages) : illustrations. |
| Supplemental Content | https://purl.fdlp.gov/GPO/gpo52191 |
| Subjects |
| Other author/creator | Hallissy, James B., author. |
| Other author/creator | Dillon, James L., author. |
| Other author/creator | United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch issuing body. |
| Other author/creator | Langley Research Center, author. |
| Series | NASA technical paper ; 1552 NASA technical paper 1552. ^A367864 |
| General note | Title from title screen (viewed Sept. 22, 2014). |
| General note | "December 1979." |
| General note | "Performing organization, NASA Langley Research Center"--Technical report documentation page. |
| Bibliography note | Includes bibliographical references (pages 20-22). |
| Funding information | Sponsored by National Aeronautics and Space Administration 505-11-33-01 |
| Funding information | L-13158 |
| Issued in other form | Print version: Penland, Jim A. Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 |
| GPO item number | 0830-H-15 (online) |
| Govt. docs number | NAS 1.60:1552 |
Availability
| Library | Location | Call Number | Status | Item Actions |
|---|---|---|---|---|
| Electronic Resources | Access Content Online | ✔ Available |