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Pressure Distribution and Shock Shape Over Blunted Slender Cones at Mach Numbers From 16 to 19

Title: Pressure Distribution and Shock Shape Over Blunted Slender Cones at Mach Numbers From 16 to 19
Date: 1961
Index Abstract: Coming Soon
Photo Quality: Incomplete
Report Number: AEDC TN 61-81
Corporate Author: VKF, ARO, Inc.
Extent: 21
Identifier: AD0261846
Distribution Classification: 1
Contract: AF 40(600)-800
DoD Project: 8951
DoD Task: 89103
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
Publisher: Arnold Air Force Station, TN : Arnold Engineering Development Center, Air Force Systems Command, USAF
Provenance: IIT
Type: report
Format: 21 pages ; 28 cm.
Creator: Lewis, Clark H.