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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Year: 1957
 Month: July
 Collection: Technical Report Archive and Image Library
The aerodynamic characteristics of a body in the two-dimensional flow field of a circular-arc wing at a Mach number of 2.01

The aerodynamic characteristics of a body in the two-dimensional flow field of a circular-arc wing at a Mach number of 2.01

Date: July 2, 1957
Creator: Gapcynski, John P & Carlson, Harry W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic Loads on Tails at High Angles of Attack and Sideslip

Aerodynamic Loads on Tails at High Angles of Attack and Sideslip

Date: July 23, 1957
Creator: Polhamus, E. C. & Spahr, J. R.
Description: Results are presented for the loads and moments acting on the individual tail surfaces of a body-tail combination over a wide range of angles of attack and sideslip. The effects of forebody length and panel-panel interference on the characteristics are included. It is shown that large nonlinear variations in these loads and moments, which occur at some combinations of angle of attack and sideslip, cannot be predicted by low-angle theory. A relatively simple, but general, theoretical method for calculating these load and moment characteristics is described, and the results from this method are found to be in good agreement with experiment provided the initial positions of the forebody vortices are known. It is shown that a simple application of slender-body theory can be used to predict the side loads due to sideslip that are contributed by a vertical tail on a wide variety of wing-body-tail combinations at low angles of attack. For several configurations, changes are indicated which reduced the vertical-tail loads per unit yawing moment of each complete configuration at large angles of attack. Some results are presented on the effect of high angle of attack on the induced-flow field and tail loads due to a wing at supersonic ...
Contributing Partner: UNT Libraries Government Documents Department
Analysis of limitations imposed on one-spool ducted-fan-engine designs by compressors and turbines at flight Mach numbers of 0, 0.6, and 0.8

Analysis of limitations imposed on one-spool ducted-fan-engine designs by compressors and turbines at flight Mach numbers of 0, 0.6, and 0.8

Date: July 18, 1957
Creator: Cavicchi, Richard H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of wing loads on a flexible swept-wing jet bomber during push-pull maneuvers

Analysis of wing loads on a flexible swept-wing jet bomber during push-pull maneuvers

Date: July 23, 1957
Creator: Gainer, Patrick A & Harper, Paul W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Arrangements of jet engine and airframe for increased range

Arrangements of jet engine and airframe for increased range

Date: July 26, 1957
Creator: Luidens, Roger W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Calculated effect of some airplane handling techniques on the ground-run distance in landing on slippery runways

Calculated effect of some airplane handling techniques on the ground-run distance in landing on slippery runways

Date: July 1, 1957
Creator: Zalovik, John A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Calculation of External-store Loads and Correlation With Experiment

Calculation of External-store Loads and Correlation With Experiment

Date: July 29, 1957
Creator: Bobbitt, P. J.; Carlson, H. W. & Pearson, A. O.
Description: Calculation of external-store loads and correlation with experiment.
Contributing Partner: UNT Libraries Government Documents Department
Comparative Study of Turbofan and Turbojet Engines

Comparative Study of Turbofan and Turbojet Engines

Date: July 19, 1957
Creator: Benser, W. A.; Gabriel, D. S. & Kaufman, H. R.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of sweep on performance of compressor blade sections as indicated by swept-blade rotor, unswept-blade rotor, and cascade tests

Effect of sweep on performance of compressor blade sections as indicated by swept-blade rotor, unswept-blade rotor, and cascade tests

Date: July 1, 1957
Creator: Godwin, William R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effects at subsonic speeds of wing fences and a tail on the longitudinal characteristics of a 63 degree swept-wing fuselage combination

The effects at subsonic speeds of wing fences and a tail on the longitudinal characteristics of a 63 degree swept-wing fuselage combination

Date: July 2, 1957
Creator: Buell, Donald A & Kolbe, Carl D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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