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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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ARMYBox004RDTM3901509534342568-02
Experimental investigation of downstream flow-field properties behind a forward located sonic jet injected into transonic freestream from a body of revolution /
1275779324
NOT Available HT 10/09/2023
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095343425
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ARMYBox004RDTM3901509534343369-02
Experimental investigation of downstream flow-field properties behind a sonic jet injected into transonic free stream from a body of revolution : Series II /
1275779325
NOT Available HT 10/09/2023
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095343433
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ARMYBox004RDTM3901509534345870-04Effect of missile nose length and shape on fin effectiveness /1275779516
NOT Available HT 10/09/2023
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095343458
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ARMYBox004RDTM3901509534340970-05
Experimental investigation of a transverse jet ejecting from a flat plate into a subsonic free stream /
1275779322
NOT Available HT 10/09/2023
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095343409
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ARMYBox004RDTM3901509534346670-06
Experimental investigation of base pressure on a body of revolution at high thrust levels and free stream Mach numbers of 1.5 to 2.87 /
1275779008
NOT Available HT 10/09/2023
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095343466
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ARMYBox004RDTM3901509534341771-16Aerodynamics of longitudinally supported ring tail configurations /1275779323
NOT Available HT 10/09/2023
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095343417
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ARMYBox004RDTM3901509534347472-01 Vol. 1
Aerodynamic characteristics of wraparound fins mounted on bodies of revolution and rheir influence on the missile static stability at Mach numbers from 0.3 to 1.3 /
1275779009
NOT Available HT 10/09/2023
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095343474
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ARMYBox004RDTM3901509534348272-01 Vol. 2
Aerodynamic characteristics of wraparound fins mounted on bodies of revolution and rheir influence on the missile static stability at Mach numbers from 0.3 to 1.3 /
1275779009
NOT Available HT 10/09/2023
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095343482
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ARMYBox004RDTM3901509534344172-06
Static aerodynamic stability characteristics of a body of revolution with wraparound fins at Mach numbers from 0.5 to 1.3 /
1275779515
NOT Available HT 10/09/2023
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095343441
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ARMYBox004RDTM3901509534349072-14
Static aerodynamic stability characteristics of a body of revolution with wraparound fins at Mach numbers from 1.6 to 2.86 /
1275779010
NOT Available HT 10/09/2023
https://babel.hathitrust.org/cgi/pt?id=mdp.39015095343490
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