columbus · Compressible Boundary Layer Equations And Stagnation Point Solution With Differences In Thermal And Dynamic Boundary Layer Thicknesses Being Considered

Compressible Boundary Layer Equations And Stagnation Point Solution With Differences In Thermal And Dynamic Boundary Layer Thicknesses Being Considered

Title: Compressible Boundary Layer Equations And Stagnation Point Solution With Differences In Thermal And Dynamic Boundary Layer Thicknesses Being Considered
Date: 1961
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: ASD TR 61-107
Creator: Buck, Melving L.
Corporate Author: Aeronautical Systems Div Wright-Patterson AFB Ohio Flight Control Lab
Laboratory: Flight Dynamics Laboratory
Extent: 45
Identifier: AD0268584
Access Rights: OTS
Distribution Classification: 1
Contract: Laboratory Research - No Contract
DoD Project: 1366
DoD Task: 14017
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Full text available by request
Date Issued: 1961-08
Abstract: The abstract for this report is either unavailable or has yet to be entered
Type: report
Provenance: Lockheed Martin Missiles & Fire Control
Format: 45 pages ; 28 cm.