You limited your search to:

  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Restricted Bulletin
 Collection: Technical Report Archive and Image Library
An approximate determination of the power required to move control surfaces as related to control-booster design

An approximate determination of the power required to move control surfaces as related to control-booster design

Date: September 1, 1945
Creator: Johnson, Harold I
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of lateral shift of center of gravity on rudder deflection required for trim

Effect of lateral shift of center of gravity on rudder deflection required for trim

Date: November 1, 1944
Creator: Hunter, P A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
NACA procedure for flight tests of aileron characteristics of airplanes

NACA procedure for flight tests of aileron characteristics of airplanes

Date: July 1, 1943
Creator: Johnson, Harold I
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of methods of supporting single-thickness specimens in a fixture for determination of compressive stress-strain curves

Investigation of methods of supporting single-thickness specimens in a fixture for determination of compressive stress-strain curves

Date: May 1, 1945
Creator: Weinberger, Robert A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The longitudinal shear strength required in double-angle columns of 24S-T aluminum alloy

The longitudinal shear strength required in double-angle columns of 24S-T aluminum alloy

Date: May 1, 1943
Creator: Moggio, Edwin M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Proposal for a propeller side-force factor

Proposal for a propeller side-force factor

Date: December 1, 1943
Creator: Ribner, Herbert S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Resume of hinge-moment data for unshielded horn- balanced control surfaces

Resume of hinge-moment data for unshielded horn- balanced control surfaces

Date: June 1, 1943
Creator: Lowry, John G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A preliminary study of machine-countersunk flush rivets subjected to a combined static and alternating shear load

A preliminary study of machine-countersunk flush rivets subjected to a combined static and alternating shear load

Date: December 1, 1943
Creator: Crate, Harold
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Preliminary tank experiments with a hydrofoil on a planing-tail seaplane hull

Preliminary tank experiments with a hydrofoil on a planing-tail seaplane hull

Date: March 1, 1944
Creator: Wadlin, Kenneth L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Preliminary tests to determine the dynamic stability characteristics of various hydrofoil systems for seaplanes and surface boats

Preliminary tests to determine the dynamic stability characteristics of various hydrofoil systems for seaplanes and surface boats

Date: November 1, 1943
Creator: King, Douglas A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some notes on the determination of the stick-fixed neutral point from wind-tunnel data

Some notes on the determination of the stick-fixed neutral point from wind-tunnel data

Date: September 1, 1943
Creator: Schuldenfrei, Marvin
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some Notes on the Determination of the Stick-Free Neutral Point from Wind-Tunnel Data

Some Notes on the Determination of the Stick-Free Neutral Point from Wind-Tunnel Data

Date: February 1, 1944
Creator: Schuldenfrei, Marvin
Description: Two graphical methods are presented for determining the stick-free neutral point, and they are extensions of the methods commonly used to determine the stick-free neutral point. A mathematical formula for computing the stick-free neutral point is also given. These methods may be applied to determine approximately the increase in tail size necessary to shift the neutral point (stick fixed or free) to any desired location on an airplane having inadequate longitudinal stability.
Contributing Partner: UNT Libraries Government Documents Department
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
Preliminary investigation of the relation of the compressive strength of sheet-stiffener panels to the diameter of rivet used for attaching stiffeners to sheet

Preliminary investigation of the relation of the compressive strength of sheet-stiffener panels to the diameter of rivet used for attaching stiffeners to sheet

Date: November 1, 1944
Creator: Hickman, William A
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
Heat-capacity lag in turbine-working fluids

Heat-capacity lag in turbine-working fluids

Date: May 1, 1944
Creator: Huber, Paul W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Maximum rates of control motion obtained from ground tests

Maximum rates of control motion obtained from ground tests

Date: May 1, 1944
Creator: Beeler, De E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Maximum lift coefficients of airplanes based on sum of wing and tail areas

Maximum lift coefficients of airplanes based on sum of wing and tail areas

Date: March 1, 1944
Creator: Ankenbruck, Herman O
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
Effect of variation in diameter and pitch of rivets on compressive strength of panels with Z-section stiffeners I : panels with close stiffener spacing that fail by local buckling

Effect of variation in diameter and pitch of rivets on compressive strength of panels with Z-section stiffeners I : panels with close stiffener spacing that fail by local buckling

Date: August 1, 1945
Creator: Hickman, William A
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
A positive-replica technique for examining finished metal surfaces and its application to aircraft engine cylinders

A positive-replica technique for examining finished metal surfaces and its application to aircraft engine cylinders

Date: September 1, 1944
Creator: Clark, Thomas P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Relative effects of cylinder-head and inlet-mixture temperatures upon knock limits of fuels

Relative effects of cylinder-head and inlet-mixture temperatures upon knock limits of fuels

Date: October 1, 1944
Creator: Hensley, Reece V
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The knock-limited performance of several fuels blended with S-2 reference fuel

The knock-limited performance of several fuels blended with S-2 reference fuel

Date: November 1, 1944
Creator: Alquist, Henry E
Description: None
Contributing Partner: UNT Libraries Government Documents Department