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DTIC AD0775744: Prediction of Aircraft Ground Performance by Evaluation of Ground Vehicle Rut Depths
Two single aircraft tires (20-20, 22-PR and 49-17, 26-PR) and three standard military trucks were tested under towed (nonpowered, nonbraked) and self-powered conditions, respectively, in buckshot clay test beds whose strengths ranged from about 110 to 600 cone index…. This item belongs to: texts/dticarchive. This item has files of the following types: Abbyy GZ, Archive…
DTIC AD0775834: Helicopter Transmission Modularization and Maintainability Analysis
The objective of the transmission modularization analysis was to develop a methodology to evaluate helicopter transmission modularization and to demonstrate the feasibility, methods, design criteria, and cost effectiveness of modularization…. This item belongs to: texts/dticarchive. This item has files of the following types: Abbyy GZ, Archive BitTorrent, DjVuTXT, Djvu XML, Item Tile, Metadata, Scandata, Single…
DTIC AD0775744: Prediction of Aircraft Ground Performance by Evaluation of Ground Vehicle Rut Depths
Two single aircraft tires (20-20, 22-PR and 49-17, 26-PR) and three standard military trucks were tested under towed (nonpowered, nonbraked) and self-powered conditions, respectively, in buckshot clay test beds whose strengths ranged from about 110 to 600 cone index…. This item belongs to: texts/dticarchive. This item has files of the following types: Abbyy GZ, Archive…
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DTIC AD0775615: Catapult Fatigue Test of the Model C-2A Airplane
A laboratory fatigue test was performed on a C-2A airframe to determine whether the airframe could sustain the effects of 3000 catapult launches. A total of 6000 catapult launch cycles were applied to the airframe with no structural failures…. This item belongs to: texts/dticarchive. This item has files of the following types: Abbyy GZ, Archive…
DTIC AD0775615: Catapult Fatigue Test of the Model C-2A Airplane
A laboratory fatigue test was performed on a C-2A airframe to determine whether the airframe could sustain the effects of 3000 catapult launches. A total of 6000 catapult launch cycles were applied to the airframe with no structural failures…. This item belongs to: texts/dticarchive. This item has files of the following types: Abbyy GZ, Archive…
DTIC AD0775744: Prediction of Aircraft Ground Performance by Evaluation of Ground Vehicle Rut Depths
Two single aircraft tires (20-20, 22-PR and 49-17, 26-PR) and three standard military trucks were tested under towed (nonpowered, nonbraked) and self-powered conditions, respectively, in buckshot clay test beds whose strengths ranged from about 110 to 600 cone index…. This item belongs to: texts/dticarchive. This item has files of the following types: Abbyy GZ, Archive…
DTIC AD0775577: High Power Dye Lasers
The report describes the operation of a high power, repetitively pulsed, flashlamp pumped dye laser. To date an average power of 39 watts at a repetition rate of 100 Hz has been obtained. The techniques employed should be scalable to higher power and higher repetition rate…. This item belongs to: texts/dticarchive. This item has files…
DTIC AD0775577: High Power Dye Lasers
The report describes the operation of a high power, repetitively pulsed, flashlamp pumped dye laser. To date an average power of 39 watts at a repetition rate of 100 Hz has been obtained. The techniques employed should be scalable to higher power and higher repetition rate…. This item belongs to: texts/dticarchive. This item has files…
DTIC AD0775615: Catapult Fatigue Test of the Model C-2A Airplane
A laboratory fatigue test was performed on a C-2A airframe to determine whether the airframe could sustain the effects of 3000 catapult launches. A total of 6000 catapult launch cycles were applied to the airframe with no structural failures…. This item belongs to: texts/dticarchive. This item has files of the following types: Abbyy GZ, Archive…