You limited your search to:

  Partner: UNT Libraries Government Documents Department
 Resource Type: Report
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
High-speed aerodynamic characteristics of a lateral-control model I : NACA 0012-64 section with 20-percent-chord plain aileron and 0 degree and 45 degrees sweepback

High-speed aerodynamic characteristics of a lateral-control model I : NACA 0012-64 section with 20-percent-chord plain aileron and 0 degree and 45 degrees sweepback

Date: September 27, 1948
Creator: Anderson, Joseph L & Krumm, Walter J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
High-speed aerodynamic characteristics of a lateral-control model II : modified NACA 0012-64 section with a 26.6-percent-chord, plain, trailing-edge aileron; wing unswept and swept back 45 degrees

High-speed aerodynamic characteristics of a lateral-control model II : modified NACA 0012-64 section with a 26.6-percent-chord, plain, trailing-edge aileron; wing unswept and swept back 45 degrees

Date: March 15, 1950
Creator: Krumm, Walter J & Anderson, Joseph L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
High-speed aerodynamic characteristics of a lateral-control model III : section characteristics, fence studies, and tabulated pressure coefficients with modified NACA 0012-64 section, 26.6-percent-chord, plain aileron, 0 and 45 degree sweepback

High-speed aerodynamic characteristics of a lateral-control model III : section characteristics, fence studies, and tabulated pressure coefficients with modified NACA 0012-64 section, 26.6-percent-chord, plain aileron, 0 and 45 degree sweepback

Date: November 22, 1950
Creator: Krumm, Walter J & Cleary, Joseph W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
High-speed aerodynamic characteristics of a model tail plane with modified NACA 65-010 sections and 0 degree and 45 degrees sweepback

High-speed aerodynamic characteristics of a model tail plane with modified NACA 65-010 sections and 0 degree and 45 degrees sweepback

Date: January 12, 1948
Creator: Anderson, Joseph L & Martin, Andrew
Description: None
Contributing Partner: UNT Libraries Government Documents Department
High-speed aerodynamic characteristics of four thin NACA 63-series airfoils

High-speed aerodynamic characteristics of four thin NACA 63-series airfoils

Date: December 31, 1947
Creator: Ilk, Richard J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
High-speed aerodynamic characteristics of horn and overhang balances on a full-scale elevator

High-speed aerodynamic characteristics of horn and overhang balances on a full-scale elevator

Date: February 27, 1948
Creator: Cleary, Joseph W & Krumm, Walter J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The high-speed aerodynamic effects of modifications to the wing and wing-fuselage intersection of an airplane model with the wing swept back 35 degrees

The high-speed aerodynamic effects of modifications to the wing and wing-fuselage intersection of an airplane model with the wing swept back 35 degrees

Date: February 18, 1948
Creator: Boddy, Lee E & Morrill, Charles P , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
High-speed aircraft

High-speed aircraft

Date: May 1, 1934
Creator: Schrenk, M
Description: This report details the designs of high-speed aircraft from various countries from 1931 on, with special emphasis on the United States and Germany.
Contributing Partner: UNT Libraries Government Documents Department
High-speed cascade tests of a blade section designed for typical hub conditions of high-flow transonic rotors

High-speed cascade tests of a blade section designed for typical hub conditions of high-flow transonic rotors

Date: September 28, 1955
Creator: Savage, Melvyn; Felix, A Richard & Emery, James C
Description: None
Contributing Partner: UNT Libraries Government Documents Department