columbus · A Method of Calculating Turbulent-Boundary-Layer Growth at Hypersonic Mach Numbers

A Method of Calculating Turbulent-Boundary-Layer Growth at Hypersonic Mach Numbers

Title: A Method of Calculating Turbulent-Boundary-Layer Growth at Hypersonic Mach Numbers
Date: 1959
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: AEDC TR 59-3
Creator: Sivells, James C.; Payne, Robert G.
Corporate Author: GDF, ARO, Inc.
Extent: 50
Identifier: AD0208774
Distribution Classification: 1
Contract: AF 40(600)-700
DoD Project: None Given
DoD Task: None Given
DTIC Record Exists: Yes
Distribution Change Authority Correspondence: AEDC LTR
Distribution Change Action Date: 4/7/2003
Report Availability: Full text available by request
Date Issued: 1959-03
Abstract: The abstract for this report is either unavailable or has yet to be entered
Publisher: Arnold Air Force Station, TN : Arnold Engineering Development Center, Air Research and Development Command, USAF
Provenance: IIT
Type: report
Format: 50 pages ; 28 cm.