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Free-flight investigation at supersonic speeds of the stability and drag of a 79 deg clipped delta boost-glide configuration including an analog study of coupled motions during the flight
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1961 |
| Description | Supersonic free-flight test of delta boost-glide figure with analog study of coupled motions |
| File Size | 7799776 |
| Page Count | 61 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630004031 |
| Archival Resource Key | ark:/13960/t0dv68d9f |
| Language | English |
| Publisher Date | 1961-01-01 |
| Access Restriction | Open |
| Subject Keyword | Free Flight Aerodynamic Characteristics Delta Wing Boost Glide Supersonic Speed Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |