columbus · The Calculation of Pressure on Slender Airplanes in Subsonic and Supersonic Flow

The Calculation of Pressure on Slender Airplanes in Subsonic and Supersonic Flow

Title: The Calculation of Pressure on Slender Airplanes in Subsonic and Supersonic Flow
Date: 1953
Index Abstract: Limited
Photo Quality: Undetermined
Report Number: NACA TN 2900
Creator: Heaslet, Max A.; Lomax, Harvard
Corporate Author: Ames Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Extent: 29
PB Number: PB108786
Identifier: AD0002873
Access Rights: Unknown
Distribution Classification: 2
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Distribution Conflict: Yes
Report Availability: Not available via Contrails
Date Issued: 1953-03
Abstract: The abstract for this report is either unavailable or has yet to be entered
Index In: PB/AD Index
Type: report