This system will be undergoing maintenance Tuesday, December 6 from 9AM to 12PM CST.

  You limited your search to:

  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Wartime Reports
 Collection: Technical Report Archive and Image Library
Numerical Evaluation of the Wake-Survey Equations for Subsonic Flow Including the Effect of Energy Addition

Numerical Evaluation of the Wake-Survey Equations for Subsonic Flow Including the Effect of Energy Addition

Date: November 1, 1945
Creator: Baal, Donald D. & Mourhess, Mary J.
Description: No abstract available.
Contributing Partner: UNT Libraries Government Documents Department
Analysis of heat and compressibility effects in internal flow systems and high-speed tests of a ram-jet system

Analysis of heat and compressibility effects in internal flow systems and high-speed tests of a ram-jet system

Date: September 1942
Creator: Baals, Donald D
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
Wind-tunnel investigation of a high-critical-speed fuselage scoop including the effects of boundary layer

Wind-tunnel investigation of a high-critical-speed fuselage scoop including the effects of boundary layer

Date: February 1, 1945
Creator: Baals, Donald D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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
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
Smoking characteristics of various fuels as determined by open-cup and laboratory-burner smoke tests

Smoking characteristics of various fuels as determined by open-cup and laboratory-burner smoke tests

Date: September 1, 1945
Creator: Barnett, Henry C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of air flow in right-angle elbows in a rectangular duct

Investigation of air flow in right-angle elbows in a rectangular duct

Date: October 1, 1941
Creator: Bartlett, Walter A , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel tests of a dual-rotating propeller having one component locked or windmilling

Wind-tunnel tests of a dual-rotating propeller having one component locked or windmilling

Date: January 1, 1945
Creator: Bartlett, Walter A , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Shear tests on DuPont explosive rivets with the countersunk head milled flush after expansion

Shear tests on DuPont explosive rivets with the countersunk head milled flush after expansion

Date: May 1, 1943
Creator: Bartone, Leonard M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tensile Tests of NACA and Conventional Machine- Countersunk Flush Rivets

Tensile Tests of NACA and Conventional Machine- Countersunk Flush Rivets

Date: October 1, 1944
Creator: Bartone, Leonard M. & Mandel, Merven W.
Description: An investigation was conducted to determine and compare the tensile strength of NACA and conventional machine-countersunk flush rivets of several rivet-head angles and varying countersunk depth. The results of the investigation are presented in the form of curves that show the variation of the tensile strength of the rivet with the ratio of the sheet thickness to the rivet diameter. For the same rivet-head angle and for a given angle of c/d, the NACA rivets developed higher tensile strength than the conventional rivets.
Contributing Partner: UNT Libraries Government Documents Department
The NACA impact basin and water landing tests of a float model at various velocities and weights

The NACA impact basin and water landing tests of a float model at various velocities and weights

Date: August 1, 1944
Creator: Batterson, Sidney A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 3 degree trim and with a 22 1/2 degree angle of dead rise

Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 3 degree trim and with a 22 1/2 degree angle of dead rise

Date: February 1, 1945
Creator: Batterson, Sidney A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 12 degree trim and with a 22-1/2 degree angle of dead rise

Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 12 degree trim and with a 22-1/2 degree angle of dead rise

Date: February 1, 1946
Creator: Batterson, Sidney A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight measurements by various methods of the drag characteristics of the XP-51 airplane

Flight measurements by various methods of the drag characteristics of the XP-51 airplane

Date: June 1, 1946
Creator: Beadle, Dorothy E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Fatigue characteristics of spot-welded 24S-T aluminum alloy

Fatigue characteristics of spot-welded 24S-T aluminum alloy

Date: June 1, 1943
Creator: Beaver, W. W.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Boundary-Layer Transition on the N.A.C.A. 0012 and 23012 Airfoils in the 8-Foot High-Speed Wind Tunnel

Boundary-Layer Transition on the N.A.C.A. 0012 and 23012 Airfoils in the 8-Foot High-Speed Wind Tunnel

Date: January 1, 1940
Creator: Becker, John V
Description: None
Contributing Partner: UNT Libraries Government Documents Department