Inhibition of flow separation at high speed. Vol. IV, Calculation of nonadiabatic laminar boundary layers on conical compression surfaces / Frederick K. Goodwin and Larry L. Lynes.
The purpose of the report is to extend other work to configurations representative of axisymmetric compression spikes. The analysis is developed and a computer program written for a spike which consists of a conical nose on which separation occurs followed by a compression surface. No data were foun...
| Uniform Title: | Technical report (Air Force Flight Dynamics Laboratory (U.S.)) ;
AFFDL-TR-68-119. |
|---|---|
| Main Author: | |
| Other Authors: | |
| Language: | English |
| Published: |
Wright-Patterson Air Force Base, OH :
Air Force Flight Dyanmics Laboratory, Air Force Systems Command,
1969.
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| Series: | Technical report (Air Force Flight Dynamics Laboratory (U.S.)) ;
AFFDL-TR-68-119. |
| Subjects: | |
| Physical Description: | ix, 44 pages. |
| Variant Title: |
Calculation of nonadiabatic laminar boundary layers on conical compression surfaces. |
| Format: | Government Document Microfilm Book |
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