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Box No.Barcode No.Item No.SuffixTitle
Print OCLC No.
Online OCLC No.
Serial InfoComments
HT/UNT Status
HT/UNT URL
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AirForceBox019AFFDLTDR3901509533553864-002Part II
Pressure and heat transfer measurements for Mach 8 flows over a blunt pyramidal configuration with aerodynamic controls /
1043670533
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AirForceBox019AFFDLTDR3901509533568664-002Part III
Pressure and heat transfer measurements for Mach 8 flows over a blunt pyramidal configuration with aerodynamic controls /
1043670533
4
AirForceBox019AFFDLTDR3901509533583564-002Part IV
Pressure and heat transfer measurements for Mach 8 flows over a blunt pyramidal configuration with aerodynamic controls /
1043670533
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UWASHBox004AFFDL-TDR3901510485613664-006
Panel flutter analyses and experiments in the Mach number range of 5.0 to 10.0 /
1527918931
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AirForceBox019AFFDLTDR3901509533554664-007
Calculation of nonlinear supersonic conical flows by the method of integral relations /
401725833
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AirForceBox019AFFDLTDR3901509533569464-010
Static aerodynamic characteristics at Mach 5 and 8 of an aerodynamically controllable winged re-entry configuration : part of an investigation of hypersonic flow separation and control characteristics /
1109637071
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AirForceBox019AFFDLTDR3901509533584364-016Part I
Nonlinear thermoelastic effects on hypersonic stability and control. Aerodynamics / Part 1, Volume 2 :
1109486521Volume 2
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AirForceBox019AFFDLTDR3901509533465564-017
Effect of surface perturbations on the pressure distributions about blunt two-dimensional bodies at high Mach numbers /
664673087
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AirForceBox019AFFDLTDR3901509533466364-035
Study and exploratory free-flight investigation of deployable aerodynamic decelerators operating at high attitudes and at high Mach numbers /
1243007712Volume 1
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AirForceBox019AFFDLTDR3901509533467164-070Aircraft motion analysis /67404305
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AirForceBox019AFFDLTDR3901509533468964-082
Conical thin-shock-layer theory uniformly valid in the entropy layer /
1109570386
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AirForceBox019AFFDLTDR3901509533480464-092
Hypersonic blunt body similitude in a perfect gas /
1243007965
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AirForceBox019AFFDLTDR3901509533481264-120
Pressure and heat transfer measurements for Mach 21 flows over a blunt pyramidal configuration with aerodynamic controls : part of an investigation of hypersonic flow separation and control characteristics /
669774856
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AirForceBox019AFFDLTDR3901509533482064-124
Pressure measurements at Mach 8 on an aerodynamically controllable winged re-entry configuration : part of an investigation of hypersonic flow separation and control characteristics /
1109540347
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AirForceBox019AFFDLTDR3901509533483864-128
Aerodynamic characteristics and flap loads for a blunt pyramidal configuration at Mach 5 and 8 : part of an investigation of hypersonic flow separation and control characteristics /
1243007966
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AirForceBox019AFFDLTDR3901509533469764-142
Heat transfer measurements at Mach 8 on an aerodynamically controllable winged re-entry configuration : part of an investigation of hypersonic flow separation and control characteristics /
54806126
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AirForceBox019AFFDLTDR3901509533484664-144
Pressure and heat transfer measurements at mach 13 and 19 for flows ahead of ramps, over expansion corners, and past fin-plate combinations : part of an investigation of hypersonic flow separation and control characteristics /
1109506493
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