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Box No.Barcode/UNT NumberReport No.SuffixTitlePrint OCLC No.
Electr. OCLC No.
Serial Info
HT/UNT Status
HT/UNT-LinksNotes
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AECBox158USAAMRDLTR3901509532791572-43
Investigation of the dissipation of the tip vortex of a rotor blade by mass injection /
1267634061
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AECBox158USAAMRDLTR3901509532792372-67
Mathematical model of unsteady aerodynamics and radial flow for application to helicopter rotors : final report /
641457860
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AECBox158USAAMRDLTR3901509532793173-02
Investigation of the suction system and boundary-layer characteristics on a high-lift, BLC L-19 test aircraft /
17255292
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AECBox158USAAMRDLTR3901509532794973-34 AVol. 1Summary of propeller design procedures and data /63979271
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AECBox158USAAMRDLTR3901509532795673-45
Vortex modification by mass injection and by tip geometry variation /
1267634060
7
AECBox158USAAMRDLTR3901509532796473-84
Analytical investigation of aerodynamic stability of helical vortices shed from hovering rotor /
1267633985
8
AECBox158USAAMRDLTR3901509532797277-45 A-BVol. 1
Aerodynamic design and analysis of propellers for mini-remotely piloted air vehicles /
1267633984
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AECBox158USAAMRDLTR3901509532798077-45 A-BVol. 2
Aerodynamic design and analysis of propellers for mini-remotely piloted air vehicles /
1267633984
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