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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Year: 1957
 Month: June
 Collection: Technical Report Archive and Image Library
Aerodynamic characteristics of missile configurations with wings of low aspect ratio for various combinations of forebodies, afterbodies, and nose shapes for combined angles of attack and sideslip at a Mach number of 2.01

Aerodynamic characteristics of missile configurations with wings of low aspect ratio for various combinations of forebodies, afterbodies, and nose shapes for combined angles of attack and sideslip at a Mach number of 2.01

Date: June 25, 1957
Creator: Robinson, Ross B
Description: An investigation has been made in the Langley 4-by-4-foot supersonic pressure tunnel to determine the aerodynamic characteristics of a series of missile configurations having low-aspect-ratio wings at a Mach number of 2.01. The effects of wing plan form and size, length-diameter ratio, forebody and afterbody length, boattailed and flared afterbodies, and component force and moment data are presented for combined angles of attack and sideslip to about 28 degrees. No analysis of the data was made in this report.
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic Heating and Boundary-layer Transition on a 1/10-power nose shape in free flight at Mach numbers up to 6.7 and Free-stream Reynolds numbers up tp 16 x 10(exp 6)

Aerodynamic Heating and Boundary-layer Transition on a 1/10-power nose shape in free flight at Mach numbers up to 6.7 and Free-stream Reynolds numbers up tp 16 x 10(exp 6)

Date: June 17, 1957
Creator: Garland, Benjamine J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamics of Oscillating Control Surfaces at Transonic Speeds

Aerodynamics of Oscillating Control Surfaces at Transonic Speeds

Date: June 17, 1957
Creator: Clevenson, S. A.
Description: Aerodynamic forces and moments of oscillating control surfaces at transonic speeds.
Contributing Partner: UNT Libraries Government Documents Department
Altitude starting tests of a small solid propellant rocket

Altitude starting tests of a small solid propellant rocket

Date: June 21, 1957
Creator: Krawczoner, E. M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analyses for turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine

Analyses for turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine

Date: June 18, 1957
Creator: Morris, James F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analyses for turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine

Analyses for turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine

Date: June 18, 1957
Creator: Morris, J. F.
Description: Turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine.
Contributing Partner: UNT Libraries Government Documents Department
Analysis of Meteorological Tower Data, April 1950 - March 1952, Brookhaven National Laboratory

Analysis of Meteorological Tower Data, April 1950 - March 1952, Brookhaven National Laboratory

Date: June 1957
Creator: Singer, Irving A. & Raynor, Gilbert S.
Description: Report issued by the Brookhaven National Laboratory discussing data collected from two BNL meteorological towers. As stated in the introduction, "results are presented in graphic form rather than tabular form" (p. 1). This report includes tables, maps, illustrations, and photographs.
Contributing Partner: UNT Libraries Government Documents Department
Analysis of two-spool turboprop-engine characteristics

Analysis of two-spool turboprop-engine characteristics

Date: June 3, 1957
Creator: Davison, Elmer H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical Investigation of Fuel-cooled Turbine Blades With Return-flow Type of Finned Coolant Passages

Analytical Investigation of Fuel-cooled Turbine Blades With Return-flow Type of Finned Coolant Passages

Date: June 26, 1957
Creator: Nachtigall, A. J.
Description: Fuel-cooled turbine blades with return-flow type of finned coolant passages.
Contributing Partner: UNT Libraries Government Documents Department
Analytical investigation of fuel-cooled turbine blades with return-flow type of finned coolant passages

Analytical investigation of fuel-cooled turbine blades with return-flow type of finned coolant passages

Date: June 26, 1957
Creator: Nachtigall, Alfred J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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