You limited your search to:

  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Restricted Bulletin
 Collection: Technical Report Archive and Image Library
Some strength tests of stiffened curved sheets loaded in shear

Some strength tests of stiffened curved sheets loaded in shear

Date: April 1, 1944
Creator: Chiarito, Patrick T
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Spinning of large airplanes

Spinning of large airplanes

Date: October 1, 1944
Creator: Seidman, Oscar
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Static-pressure error of an airspeed installation on an airplane in high-speed dives and pullouts

Static-pressure error of an airspeed installation on an airplane in high-speed dives and pullouts

Date: February 1, 1946
Creator: Wood, Clotaire
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A study of the effects of radii of gyration and altitude on aileron effectiveness at high speed

A study of the effects of radii of gyration and altitude on aileron effectiveness at high speed

Date: April 1, 1943
Creator: Fehlner, Leo F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tables and charts for the evaluation of profile drag from wake surveys at high subsonic speeds

Tables and charts for the evaluation of profile drag from wake surveys at high subsonic speeds

Date: July 1, 1945
Creator: Katzoff, S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Test data on the shear strength of joints assembled with round-head and brazier-head rivets

Test data on the shear strength of joints assembled with round-head and brazier-head rivets

Date: June 1, 1943
Creator: Schuette, Evan H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tests of 10-inch 24S-T aluminum-alloy shear panels with 1-1/2-inch holes I

Tests of 10-inch 24S-T aluminum-alloy shear panels with 1-1/2-inch holes I

Date: June 1, 1943
Creator: Levin, L Ross
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tests of 10 inch 24S-T aluminum-alloy shear panels with 1-1/2 inch holes II : panels having holes with notched edges

Tests of 10 inch 24S-T aluminum-alloy shear panels with 1-1/2 inch holes II : panels having holes with notched edges

Date: April 1, 1944
Creator: Levin, L Ross
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tests of beams having webs with large circular lightening holes

Tests of beams having webs with large circular lightening holes

Date: February 1, 1944
Creator: Levin, L Ross
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tests of hydraulically expanded rivets

Tests of hydraulically expanded rivets

Date: March 1, 1944
Creator: Schuette, Evan H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Theoretical and experimental dynamic loads for a prismatic float having an angle of dead rise of 22-1/2 degrees

Theoretical and experimental dynamic loads for a prismatic float having an angle of dead rise of 22-1/2 degrees

Date: July 1, 1945
Creator: Mayo, Wilbur L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Thermodynamic design of double-panel, air-heated windshields for ice prevention

Thermodynamic design of double-panel, air-heated windshields for ice prevention

Date: June 1, 1943
Creator: Kushnick, Jerome L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The use of geared spring tabs for elevator control

The use of geared spring tabs for elevator control

Date: February 1, 1945
Creator: Phillips, William H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Use of Internal Coolant as a Means of Permitting Increase in Engine Take-Off Power

Use of Internal Coolant as a Means of Permitting Increase in Engine Take-Off Power

Date: January 1, 1944
Creator: Rothrock, Addison M
Description: Engine tests, together with estimates made at Langley Memorial Aeronautical Laboratory, indicate that a 25-percent increase in take-off power can be obtained with present-day aircraft engines without increasing either the knock limit of the fuel or the external cooling requirements of the engine. This increase in power with present fuels and present external cooling is made possible through the use of an internal coolant inducted through the inlet manifold. Estimates on aircraft indicate that this 25-percent increase in power will permit an approximate usable increase of 8.5 percent in the take-off load of existing military airplanes. This increase in load is equivalent to an increase in the weight of gasoline normally carried of between 30 and 65 percent.
Contributing Partner: UNT Libraries Government Documents Department
Use of stagnation temperature in calculating rate of heat transfer in aircraft heat exchangers

Use of stagnation temperature in calculating rate of heat transfer in aircraft heat exchangers

Date: October 1, 1943
Creator: Wood, George P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Use of variable-ratio geared tabs to improve stick-force characteristics in turning flight

Use of variable-ratio geared tabs to improve stick-force characteristics in turning flight

Date: October 1, 1945
Creator: Kleckner, Harold F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Use of water injection to decrease gasoline consumption in an aircraft engine cruising at high power

Use of water injection to decrease gasoline consumption in an aircraft engine cruising at high power

Date: August 1, 1944
Creator: White, H Jack
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 6 degrees and 9 degrees trim and a 22-1/2 degree angle of dead rise

Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 6 degrees and 9 degrees trim and a 22-1/2 degree angle of dead rise

Date: February 1, 1946
Creator: Stewart, Thelma
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
Wind-tunnel tests of a piston-type control booster on an airfoil and aileron model

Wind-tunnel tests of a piston-type control booster on an airfoil and aileron model

Date: November 1, 1943
Creator: Mendelsohn, Robert A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
XC-35 gust research project analysis of gust measurements

XC-35 gust research project analysis of gust measurements

Date: April 1, 1944
Creator: Moskovitz, A I
Description: None
Contributing Partner: UNT Libraries Government Documents Department
XC-35 gust research project characteristics of vertical drafts and associated vertical gust velocities within convective type clouds

XC-35 gust research project characteristics of vertical drafts and associated vertical gust velocities within convective type clouds

Date: February 1, 1945
Creator: Moskovitz, A I
Description: None
Contributing Partner: UNT Libraries Government Documents Department