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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Year: 1957
 Collection: Technical Report Archive and Image Library
Comparison and evaluation of two model techniques used in predicting bomb-release motions

Comparison and evaluation of two model techniques used in predicting bomb-release motions

Date: December 27, 1957
Creator: Carlson, H. W.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Comparison and Evaluation of Two Model Techniques Used in Predicting Bomb-Release Motions

Comparison and Evaluation of Two Model Techniques Used in Predicting Bomb-Release Motions

Date: December 27, 1957
Creator: Carlson, Harry W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Experimental hinge moments on two freely oscillating trailing-edge controls hinged at 55 percent control chord

Experimental hinge moments on two freely oscillating trailing-edge controls hinged at 55 percent control chord

Date: December 27, 1957
Creator: Martz, C William
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Pressure measurements on an afterbody behind various blunt nose shapes at a Mach number of 2

Pressure measurements on an afterbody behind various blunt nose shapes at a Mach number of 2

Date: December 27, 1957
Creator: Speegle, K. C.
Description: No abstract available.
Contributing Partner: UNT Libraries Government Documents Department
Supplementary investigation in the Langley 20-foot free-spinning tunnel of a 1/20-scale model of the Douglas F4D-1 airplane with external wing fuel tanks : TED No. NACA AD 3116

Supplementary investigation in the Langley 20-foot free-spinning tunnel of a 1/20-scale model of the Douglas F4D-1 airplane with external wing fuel tanks : TED No. NACA AD 3116

Date: December 27, 1957
Creator: Bowman, James S , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Heat-Transfer and Pressure Measurements from a Flight Test of a 1/18-Scale Model of the Titan Intercontinental Ballistic Missile up to a Mach Number of 3.95 and Reynolds Number Per Foot of 23 by 10 to the 6Th Power

Heat-Transfer and Pressure Measurements from a Flight Test of a 1/18-Scale Model of the Titan Intercontinental Ballistic Missile up to a Mach Number of 3.95 and Reynolds Number Per Foot of 23 by 10 to the 6Th Power

Date: December 19, 1957
Creator: Chauvin, L. T.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Heat-transfer and pressure measurements from a flight test of a 1/18-scale model of the Titan intercontinental ballistic missile up to a Mach number of 3.95 and Reynolds number per foot of 23 x 10(exp 6) : COORD. No. AF-AM-70

Heat-transfer and pressure measurements from a flight test of a 1/18-scale model of the Titan intercontinental ballistic missile up to a Mach number of 3.95 and Reynolds number per foot of 23 x 10(exp 6) : COORD. No. AF-AM-70

Date: December 19, 1957
Creator: Graham, John B , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effects of boundary-layer separation over bodies of revolution with conical tail flares

The effects of boundary-layer separation over bodies of revolution with conical tail flares

Date: December 12, 1957
Creator: Dennis, David H
Description: The magnitude and the effects of boundary-layer separation on normal-force-curve slopes, centers of pressure, pressure distributions, and lift and drag coefficients were determined for various bodies of revolution with conical tail flares at Mach numbers from 3.0 to 6.3. Some of the experimental results are compared to theoretical predictions of the aerodynamic characteristics of the bodies.
Contributing Partner: UNT Libraries Government Documents Department
Experimental investigation of the simulation of atmospheric entry of ballistic missiles

Experimental investigation of the simulation of atmospheric entry of ballistic missiles

Date: December 12, 1957
Creator: Neice, Stanford E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
In-flight Gains Realized by Modifying a Twin Side-inlet Induction System

In-flight Gains Realized by Modifying a Twin Side-inlet Induction System

Date: December 12, 1957
Creator: Saltzman, E. J.
Description: Modification of twin side-inlet induction system and in-flight gains.
Contributing Partner: UNT Libraries Government Documents Department
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