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 Serial/Series Title: NACA Advanced Confidential Report
 Serial/Series Title: NACA Wartime Reports
 Collection: National Advisory Committee for Aeronautics Collection
Supersonic-tunnel tests of projectiles in Germany and Italy

Supersonic-tunnel tests of projectiles in Germany and Italy

Date: October 1, 1945
Creator: Ferri, Antonio
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Comparison of calculated and experimental propeller characteristics for four-, six-, and eight-blade single-rotating propellers

Comparison of calculated and experimental propeller characteristics for four-, six-, and eight-blade single-rotating propellers

Date: February 1, 1944
Creator: Crigler, John L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of the lift coefficient on propeller flutter

Effect of the lift coefficient on propeller flutter

Date: July 1, 1945
Creator: Regier, Arthur A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Considerations of wake-excited vibratory stress in a pusher propeller

Considerations of wake-excited vibratory stress in a pusher propeller

Date: February 1, 1944
Creator: Miller, Mason, F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Simple curves for determining the effects of compressibility on pressure drop through radiators

Simple curves for determining the effects of compressibility on pressure drop through radiators

Date: September 1, 1944
Creator: Baals, Donald D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigations on laminar boundary-layer stability and transition on curved boundaries

Investigations on laminar boundary-layer stability and transition on curved boundaries

Date: May 1, 1946
Creator: Liepmann, Hans W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Theory and application of hot-wire instruments in the investigation of turbulent boundary layers

Theory and application of hot-wire instruments in the investigation of turbulent boundary layers

Date: March 1, 1946
Creator: Klebanoff, P S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Parameters determining performance of supersonic pilotless airplanes powered by ram-compression power planes

Parameters determining performance of supersonic pilotless airplanes powered by ram-compression power planes

Date: June 1, 1946
Creator: Hill, Paul R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Knock-limited power outputs from a CFR engine using internal coolants II : six aliphatic amines

Knock-limited power outputs from a CFR engine using internal coolants II : six aliphatic amines

Date: October 1, 1945
Creator: Evvard, John C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A method for the calculation of external lift, moment, and pressure drag of slender open-nose bodies of revolution at supersonic speeds

A method for the calculation of external lift, moment, and pressure drag of slender open-nose bodies of revolution at supersonic speeds

Date: March 1, 1946
Creator: Parker, Hermon M
Description: None
Contributing Partner: UNT Libraries Government Documents Department