columbus · Investigation of Free-Stream Pressure and Stagnation Pressure Measurement from Transonic and Supersonic Aircraft: Final Report

Investigation of Free-Stream Pressure and Stagnation Pressure Measurement from Transonic and Supersonic Aircraft: Final Report

Title: Investigation of Free-Stream Pressure and Stagnation Pressure Measurement from Transonic and Supersonic Aircraft: Final Report
Date: 1958
Index Abstract: Limited
Photo Quality: Incomplete
Report Number: WADC TR 55-238
Creator: Smetana, Frederick O.
Corporate Author: University of Southern California Engineering Center
Laboratory: Flight Control Laboratory
Extent: 95
Identifier: AD0155645
Access Rights: ASTIA
Distribution Classification: 2
Contract: AF 33(616)-2396
DoD Task: None Given
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Not available via Contrails
DoD Project: None Given
Date Issued: 1958-04
Abstract: The abstract for this report is either unavailable or has yet to be entered
Type: report
Provenance: AFRL/VACA; Bombardier/Aero