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Barcode/UNT NumberReport No.SuffixTitlePrint OCLC No.Electr. OCLC No.Serial InfoHT/UNT StatusHT/UNT-LinksNotes
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NACARMBox0043901508648995552I25Torsion, compression, and bending tests of tubular sections machines from 75S-T6 rolled round rod /824986059885133113Available 8/17/16; NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086489955;
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NACARMBox004390150864899639D06Strategic virgin metal requirements for five aircraft gas turbine engines /824986058885133150Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086489963;
5
NACARMBox00439015086489989A50H24Flight calibration of four airspeed systems on a swept-wing airplane at Mach numbers up to 1.04 by the NACA radar-phototheodolite method /680502467885133059Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086489989;
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NACARMBox00139015086432435A51C19Analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /816702085885059961Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432435;
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NACARMBox00139015086432740A51G31aSummary of results of a wind-tunnel investigation of nine related horizontal tails /816702074885133426Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432740
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NACARMBox00439015086490292A51H10Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane 45° swept-back wing of aspect ratio 3, taper ratio 0.4 with 3-percent-thick, biconvex section /824989556885132851Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086490292
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NACARMBox00439015086489971A51H23Aerodynamic characteristics of a leading-edge slat on a 35 degree swept-back wing for Mach numbers from 0.30 to 0.88 /712649131885133182Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086489971
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NACARMBox00139015086432591A51L17aEffect of various missile characteristics on airframe frequency response /816702086885133413Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432591
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NACARMBox00139015086432443A52A18Instrumentation of the ames supersonic free-flight wind tunnel /816701709885133551Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432443
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NACARMBox00139015086432757A52D01bBoundary-layer measurements on several porous materials with suction applied /816702087885146321Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432757
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NACARMBox00139015086432609A52D24Supplementary note on modified-impact-theory calculations for bodies of revolution having minimum drag at hypersonic speeds /816702088885133449Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432609
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NACARMBox00139015086432450A52J08Downwash characteristics and vortex-sheet shape behind a 63 degree swept-back wing-fuselage combination at a Reynolds number of 6,100,000 /816690370885198677Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432450
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NACARMBox00139015086432765A53A30aEffects of compressibility on the upwash at the propeller planes of a four-engine tractor airplane configuration having a wing with 40 degrees of sweepback and an aspect ratio of 10 /816702071885146315Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432765
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NACARMBox00139015086432617A53E29Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds /816701705885059870Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432617
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NACARMBox00139015086432468A54A05Evaluation of two cooling-air ejectors in flight at transonic speeds /816701719885060110Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432468
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NACARMBox00139015086432773A54B18aInvestigation of a three-blade propeller in combination with two different spinners and an NACA D-type cowl at mach numbers up to 0.80 /816690384885133396Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432773
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NACARMBox00139015086432625A54F28On the range of applicability of the transonic area rule /130052568857368937Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432625
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NACARMBox00139015086432476A54H09Experimental and predicted longitudinal response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet /816690385885133666Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432476
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NACARMBox00539015086429787A54H23aInvestigation of the lift, center of pressure, and drag of a projectile at Mach number of 8.6 and a Reynolds number of 17 million /857063215897078899Available HT 9/12/19, Search only in HT 1/17/2017https://babel.hathitrust.org/cgi/pt?id=mdp.39015086429787
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NACARMBox00639015095100650A54K16Tracking performance of a swept-wing figher with a disturbed reticle lead-computing sight /9687983761013869817Available HT 10/17/2019, https://babel.hathitrust.org/cgi/pt?id=mdp.39015095100650
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NACARMBox00139015086432484A55A18Wave drag of arbitrary configurations in linearized flow as determined by areas and forces in oblique planes /816690386885060056Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432484
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NACARMBox00139015086432633A55B07General theory of wave-drag reduction for combinations employing quasi-cylindrical bodies with an application to swept-wing and body combinations /816701704885133438Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432633
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NACARMBox00739015095338433A55B21
Experimental investigation of two methods for reducing transonic drag of swept-wing and body combinations /
1109543318
26
NACARMBox00139015086432781A55C07Flight tests of a leading-edge area suction on a fighter-type airplane with a 35 degree sweptback wing /712654820885060467Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432781
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NACARMBox00739015095338250A55C08
Correlation of airfoil section data with the aerodynamic loads measured on a 45 degree sweptback wing model at subsonic Mach numbers /
1109593676
28
NACARMBox00739015095338268A55D08
Experimental investigation of some aerodynamic effects of a gap between wing and body of a moderately slender wing-body combination at a Mach number of 1.4 /
1109533399
29
NACARMBox00739015095338276A55D11
Investigation of the effects of an airfoil section modification on the aerodynamic characteristics at subsonic and supersonic speeds of a thin swept wing of aspect ratio 3 in combination with a body /
712672342
30
NACARMBox00739015095338284A55D12Controls for supersonic missiles /1109533581
31
NACARMBox00139015086432799A55D12aEffects of powered controls and fire-control systems on tracking accuracy /816702090885061023Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432799
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NACARMBox00739015095338102A55D14
Effects of flexibility on the longitudinal and lateral-directional response of a large airplane /
694766832
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NACARMBox00739015095338110A55D27
Experimental investigation at Mach numbers from 0 to 1.9 of trapezoidal and circular side inlets for a fighter-type airplane /
1109696276
34
NACARMBox00139015086432641A55D27aComparison at mach numbers up to 0.92 of the calculated and experimental downwash and wake characteristics at various horizonatl tail heights behind a wing with 45 degrees of sweepback /816690387885060451Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432641
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NACARMBox00139015086432492A55E11aApplication of statistical theory to beam-rider guidance in the presence of noise. [Part] 2, Modified Wiener filter theory /712697852885060413Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432492
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NACARMBox00739015095338128A55E17
Load distribution on wings and wing-body combinations at high angles of attack and supersonic speeds /
1109543156
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NACARMBox00739015095338136A55E31
Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 1.98 /
712673762
38
NACARMBox00739015095338144A55F02
Theoretical investigation of the effects of configuration changes on the center-of-pressure shift of a body-wing-tail combination due to angle of attack and Mach number at transonic and supersonic speeds /
688507834
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NACARMBox00739015095338151A55F15
Drag and rolling-moment effectiveness of trailing-edge spoilers at Mach numbers 2.2 and 5.0 /
1109555074
40
NACARMBox00739015095338169A55F16
Aerodynamic principles for the design of jet-engine induction systems /
1264098695
41
NACARMBox00739015095338292A55F21
Flight investigation at transonic speeds of a model having a triangular wing of aspect ratio 2 /
1109599127
42
NACARMBox00139015086433243A55F21aDiscussion of methods for reducing aerodynamic heating in supersonic flight /66528800885060482Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086433243
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NACARMBox00739015095338300A55F23
Preliminary experimental investigation of a variable-area, variable-internal-contraction air inlet at Mach numbers between 1.42 and 2.44 /
1109713528
44
NACARMBox00739015095338318A55F29
Fuselage side inlets : a study of some factors affecting their performance and a comparison with nose inlets /
1109638652
45
NACARMBox00139015086432153A55G11Methods for connection to revolving thermocouples /816701741885060814Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432153
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NACARMBox00739015095338441A55H09
Effects of boundary-layer separation on normal force and center of pressure of a cone-cylinder model with a large base flare at Mach numbers from 3.00 to 6.28 /
1109613947
47
NACARMBox00739015095338458A55I15
Method for simulating the atmospheric entry of long-range ballistic missiles /
713021594
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NACARMBox00139015086432948A55J21Measurement of the longitudinal moment of inertia of a flexible airplane /713023096885133700Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432948
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NACARMBox00739015095338466A55J28
Application of Tchebichef form of harmonic analysis to the calculation of zero-lift wave drag of wing-body-tail combinations /
1109546779
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NACARMBox00739015095338474A55K07
Effects of two trailing-edge controls on the aerodynamic characteristics of a rectangular wing and body combination at Mach numbers from 3.00 to 5.05 /
1109668044
51
NACARMBox00739015095338482A55K09
Force, moment, and pressure-distribution characteristics of rectangular wings at high angles of attack and supersonic speeds /
1109677894
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NACARMBox00139015086433235A55K10Influence of the body flow field on the zero-lift wave drag of wing-body combinations modified in accordance with the transonic area rule /816701732885133325Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086433235
53
NACARMBox00739015095338490A55K21
Lift, drag, and static longitudinal stability characteristics of configurations consisting of three triangular wing panels and a body of equal length at Mach numbers from 3.00 to 6.28 /
694897969
54
NACARMBox00739015095338508A55L02
Effect of boundary-layer control and inlet lip shape on the performance on a twin-scoop air-induction system at Mach numbers from 0 to 1.9 /
1109535379
55
NACARMBox00739015095338326A55L05
Aircraft configurations developing high lift-drag ratios at high supersonic speeds /
133095291
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NACARMBox00139015086433086A55L13aHeat-transfer characteristics of blunt two-and three-dimensional bodies at supersonic speeds /816702091885060772Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086433086
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NACARMBox00739015095338334A55L13b
Aerodynamics of missiles employing wings of very low aspect ratio /
1109491117
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NACARMBox00739015095338342A55L13c
Aerodynamics of bodies, wings, and wing-body combinations at high angles of attack and supersonic speeds /
1109590677
59
NACARMBox00739015095338359A55L15
Problems of performance and heating of hypersonic vehicles /
694884782
60
NACARMBox00739015095338177A55L16
Study of a symmetrical, circular, internal compression inlet /
1109633836
61
NACARMBox00739015095338185A56B21
Light diffusion through high-speed turbulent boundary layers /
66528424
62
NACARMBox00739015095338193A56B27
Investigation of the use of area suction to increase the effectiveness of trailing-edge flaps of various spans on a wing of 45 degree sweepback and aspect ratio 6 /
713034521
63
NACARMBox00739015095338201A56B27a
Method of reducing heat transfer to blunt bodies by air injection /
713037714
64
NACARMBox00739015095338219A56C01
Effects of blowing over various trailing-edge flaps on an NACA 0006 airfoil section, comparisons with various types of flaps on other airfoil sections, and an analysis of flow and power relationships for blowing systems /
713036965
65
NACARMBox00739015095338227A56C06
Change with mass-flow ratio of the cowl pressure drag of normal-shock inlets at supersonic speeds /
1109544981
66
NACARMBox00739015095338235A56D23
Use of area suction for improving the longitudinal characteristics of a thin unswept wing-fuselage model with leading- and trailing-edge flaps /
713041927
67
NACARMBox00739015095338243A56E24
Full-scale wind-tunnel tests of a 35 degree sweptback-wing airplane with high-velocity blowing over the trailing-edge flaps : longitudinal and lateral stability and control /
1109500617
68
NACARMBox00739015095338367A56F07
Simulator study of some longitudinal stability and control problems of a piloted aircraft in flights to extreme altitude and high speed /
1109549329
69
NACARMBox00739015095338375A56F12
Analysis of some parameters used in correlating blowing-type boundary-layer control data /
713047402
70
NACARMBox00739015095338383A56F15
Motion of a ballistic missile angularly misaligned with the flight path upon entering the atmosphere and its effect upon aerodynamic heating, aerodynamic loads, and miss distance /
713046698
71
NACARMBox00739015095338524A56G17
Measurements of boundary-layer transition at low speed on two bodies of revolution in a low-turbulence wind tunnel /
66528255
72
NACARMBox00739015095338532A56G19
Wind-tunnel tests of blowing boundary-layer control with jet pressure ratios up to 9.5 on the trailing-edge flaps of a 35 degree sweptback wing airplane /
713051379
73
NACARMBox00739015095338516A56G30
Flight measurements of the low-speed characteristics of a 35 degree swept-wing airplane with blowing-type boundary-layer control in the trailing-edge flaps /
713072528
74
NACARMBox00739015095338540A56H06
Subsonic lateral and longitudinal static stability characteristics up to large angles of sideslip for a triangular-wing airplane model having a ventral fin /
1109655472
75
NACARMBox00739015095337658A56H08
Large-scale wind-tunnel tests of an airplane model with a 45 degree sweptback wing of aspect ratio 2.8 with area suction applied to trailing-edge flaps and with several wing leading-edge modifications /
713075562
76
NACARMBox00739015095337666A56H27
Investigation of the lift, drag, and static-stability characteristics of a triangular-wing airplane configuration at Mach numbers from 3.00 to 6.28 /
713267011
77
NACARMBox00539015086429795A56H31Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4 /713270945897078906Available HT 10/17/2019, https://babel.hathitrust.org/cgi/pt?id=mdp.39015086429795
78
NACARMBox00739015095337674A56I05
Some experiments at high supersonic speeds on the aerodynamic and boundary-layer transition characteristics of high-drag bodies of revolution /
1109623770
79
NACARMBox00739015095337807A56L18
Effects of conical camber on the lift, drag, and pitching-moment characteristics of a triangular wing of aspect ratio 3.0 /
713295706
80
NACARMBox00739015095337815A57A02
Investigation of wing-body juncture interference effects at transonic speeds for several swept-wing and body combinations /
713316385
81
NACARMBox00739015095337823A57A24
Wind-tunnel tests of the static longitudinal characteristics at low speed of a swept-wing airplane with slotted flaps, area suction flaps, and wing leading-edge devices /
1109521413
82
NACARMBox00739015095337955A57A25
Lateral-directional aerodynamic characteristics of several coplanar triple-body missile configurations at Mach numbers from 0.6 to 1.4 /
1109543986
83
NACARMBox00739015095337963A57B11
Leading-edge contours for thin swept wings : an analysis of low-and high-speed data /
713314618
84
NACARMBox00739015095337971A57B14
Flight investigation of area-suction and blowing boundary-layer control on the trailing-edge flaps of a 35 degree swept-wing carrier-type airplane /
1109559072
85
NACARMBox00739015095337682A57C19
Air-borne target simulator for use with scope-presentation type fire-control systems /
1264098696
86
NACARMBox00739015095337831A57C25
Investigation of boundary-layer transition on flat-faced bodies of revolution at high supersonic speeds /
1109533358
87
NACARMBox00739015095337989A57D04
Analytical study of the comparative pitch-up behavior of several airplanes and correlation with pilot opinion /
713322582
88
NACARMBox00739015095337690A57D09
Flight tests of an automatic interceptor system with a tracking radar modified to minimize the interaction between antenna and interceptor motions /
1109574413
89
NACARMBox00739015095337849A57D11
Wind-tunnel tests of the static longitudinal characteristics at low speed of a swept-wing airplane with blowing flaps and leading-edge slats /
1109487411
90
NACARMBox00739015095337997A57D30
Comparison of carrier approach speeds as determined from flight tests and from pilot-operated simulator studies /
713322734
91
NACARMBox00739015095337708A57E21
Aerodynamic loads on tails at high angles and sideslip /
1109692681
92
NACARMBox00739015095337856A57E24
Investigation of axially symmetric flow over steps at transonic speeds with comparisons of estimated and experimental drag results /
713329068
93
NACARMBox00139015086432930A57F03aHeat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds /816690388885060933Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432930
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NACARMBox00139015086433227A57F06aA buffet investigation at high subsonic speeds of wing-fuselage-tail combinations having sweptback wings with NACA 64A thickness distributions, fences, a leading-edge extension, and body contouring /713325058885060498Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086433227
95
NACARMBox00539015086429803A57F06bEffects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4 /713342092897078907Available HT 10/17/2019, https://babel.hathitrust.org/cgi/pt?id=mdp.39015086429803
96
NACARMBox00739015095338003A57F26
Effects of target and missile characteristics on theoretical minimum miss distance for a beam-rider guidance system in the presence of noise /
459552600
97
NACARMBox00739015095337716A57G10
Flight investigation of the low-speed characteristics of a 35° swept-wing airplane equipped with an area-suction ejector flap and vaious wing leading-edge devices /
708264035
98
NACARMBox00739015095338391A57G16
Wing-body combinations with wings of very low aspect ratio at supersonic speeds /
1109542578
99
NACARMBox00739015095337864A57H19
Effects of a leading-edge slat and a trailing-edge split flap on the aerodynamic characteristics of a wing-fuselage combination having a nearly triangular wing of aspect ratio 2.9 at Mach numbers from 0.60 to 0.92 /
1109594580
100
NACARMBox00139015086433078A57H19aTransonic investigation of the effects of semisubmerged-store cavities and of slots on the zero-lift drag of a body of revolution /816701733885060672Available HT 10/17/2019, NOT IN HT 1/13/2014https://babel.hathitrust.org/cgi/pt?id=mdp.39015086433078
101
NACARMBox00739015095338011A57H21
Use of a leading-edge area-suction flap and leading-edge modifications to improve the high-lift characteristics of an airplane model with a wing of 45 degree sweep and aspect ratio 2.8 /
713342247