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  Partner: UNT Libraries Government Documents Department
 Collection: National Advisory Committee for Aeronautics Collection
Results 13311 - 13320 of 13,793
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Wall pressure fluctuations in a turbulent boundary layer

Wall pressure fluctuations in a turbulent boundary layer

Date: March 1, 1958
Creator: Willmarth, William W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Static longitudinal and lateral stability and control characteristics of a model of a swept-wing fighter-bomber-type airplane with a top inlet at Mach numbers from 1.6 to 2.35

Static longitudinal and lateral stability and control characteristics of a model of a swept-wing fighter-bomber-type airplane with a top inlet at Mach numbers from 1.6 to 2.35

Date: March 3, 1958
Creator: Gnos, A Vernon
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Summary of locations, extents, and intensities of turbulent areas encountered during flight investigations of the jet stream from January 7, 1957 to April 28, 1957

Summary of locations, extents, and intensities of turbulent areas encountered during flight investigations of the jet stream from January 7, 1957 to April 28, 1957

Date: March 3, 1958
Creator: Copp, Martin R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of a hot-jet exhaust on pressure distributions and external drag of several afterbodies on a single-engine airplane model at transonic speeds

Effect of a hot-jet exhaust on pressure distributions and external drag of several afterbodies on a single-engine airplane model at transonic speeds

Date: March 4, 1958
Creator: Norton, Harry T , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effects of a modified roll-command system on the flight-path stability and tracking accuracy of an automatic interceptor

The effects of a modified roll-command system on the flight-path stability and tracking accuracy of an automatic interceptor

Date: March 4, 1958
Creator: Triplett, William C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Study of exit phase of flight of a very high altitude hypersonic airplane by means of a pilot-controlled analog computer

Study of exit phase of flight of a very high altitude hypersonic airplane by means of a pilot-controlled analog computer

Date: March 4, 1958
Creator: Sherman, Windsor L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of surface roughness and extreme cooling on boundary-layer transition for 15 deg cone-cylinder in free flight at Mach numbers to 7.6

Effects of surface roughness and extreme cooling on boundary-layer transition for 15 deg cone-cylinder in free flight at Mach numbers to 7.6

Date: March 5, 1958
Creator: Rabb, L.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Experimental investigation of the effect of circumferential inlet flow distortion on the performance of a five-stage axial-flow research compressor with transonic rotors in all stages

Experimental investigation of the effect of circumferential inlet flow distortion on the performance of a five-stage axial-flow research compressor with transonic rotors in all stages

Date: March 5, 1958
Creator: Robbins, William H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Performance of a two-dimensional cascade inlet at a free-stream Mach number of 3.05 and at angles of attack of -3 degrees, 0 degrees, 3 degrees, and 6 degrees

Performance of a two-dimensional cascade inlet at a free-stream Mach number of 3.05 and at angles of attack of -3 degrees, 0 degrees, 3 degrees, and 6 degrees

Date: March 5, 1958
Creator: Woolett, Richard R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of canard surface size on stability and control characteristics of two canard airplane configuration at Mach numbers of 1.41 and 2.01

Effects of canard surface size on stability and control characteristics of two canard airplane configuration at Mach numbers of 1.41 and 2.01

Date: March 6, 1958
Creator: Spearman, M Leroy
Description: None
Contributing Partner: UNT Libraries Government Documents Department