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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Wartime Reports
 Collection: Technical Report Archive and Image Library
Wind tunnel tests of a submerged-engine fuselage design

Wind tunnel tests of a submerged-engine fuselage design

Date: October 1, 1940
Creator: Baals, Donald D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of carburetor throttle settings on the velocity distribution at the outlet of a vaned and vaneless supercharger inlet elbow

The effect of carburetor throttle settings on the velocity distribution at the outlet of a vaned and vaneless supercharger inlet elbow

Date: September 1, 1945
Creator: Baas, Edmund J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of changes in aspect ratio, side area, flight-path angle, and normal acceleration on lateral stability

Effect of changes in aspect ratio, side area, flight-path angle, and normal acceleration on lateral stability

Date: December 1, 1942
Creator: Bamber, M J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tank tests on the resistance and porpoising characteristics of three flying-boat hull models equipped with planing flaps

Tank tests on the resistance and porpoising characteristics of three flying-boat hull models equipped with planing flaps

Date: November 1, 1944
Creator: Barklie, Jean A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
High-speed aerodynamic characteristics of a four-engine bomber airplane as determined from tests of a 0.075-scale model

High-speed aerodynamic characteristics of a four-engine bomber airplane as determined from tests of a 0.075-scale model

Date: January 1, 1944
Creator: Barnes, Robert H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
High-speed aerodynamic characteristics of a four-engine transport airplane as determined from tests of a 0.075-scale model

High-speed aerodynamic characteristics of a four-engine transport airplane as determined from tests of a 0.075-scale model

Date: January 1, 1944
Creator: Barnes, Robert H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of varying percentages of exhaust gas on engine performance

Effect of varying percentages of exhaust gas on engine performance

Date: April 1, 1943
Creator: Barnett, Henry C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Estimation of F-3 and F-4 knock-limited performance ratings for ternary and quaternary blends containing triptane or other high-antiknock aviation-fuel blending agents

Estimation of F-3 and F-4 knock-limited performance ratings for ternary and quaternary blends containing triptane or other high-antiknock aviation-fuel blending agents

Date: January 1, 1948
Creator: Barnett, Henry C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An evaluation of the knock-limited performance of triptane

An evaluation of the knock-limited performance of triptane

Date: March 1, 1946
Creator: Barnett, Henry C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Lead susceptibility of paraffins, cycloparaffins, and olefins

Lead susceptibility of paraffins, cycloparaffins, and olefins

Date: May 1, 1943
Creator: Barnett, Henry C
Description: None
Contributing Partner: UNT Libraries Government Documents Department