A | B | C | D | E | F | G | H | I | J | K | L | M | N | O | P | Q | R | S | T | U | V | W | X | Y | Z | |
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1 | Barcode/UNT Number | Report No. | Suffix | Title | Print OCLC No. | Electr. OCLC No. | Serial Info | HT/UNT Status | HT/UNT-Links | Notes | ||||||||||||||||
3 | NACARMBox004 | 39015086489955 | 52I25 | Torsion, compression, and bending tests of tubular sections machines from 75S-T6 rolled round rod / | 824986059 | 885133113 | Available 8/17/16; NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086489955; | ||||||||||||||||||
4 | NACARMBox004 | 39015086489963 | 9D06 | Strategic virgin metal requirements for five aircraft gas turbine engines / | 824986058 | 885133150 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086489963; | ||||||||||||||||||
5 | NACARMBox004 | 39015086489989 | A50H24 | Flight calibration of four airspeed systems on a swept-wing airplane at Mach numbers up to 1.04 by the NACA radar-phototheodolite method / | 680502467 | 885133059 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086489989; | ||||||||||||||||||
6 | NACARMBox001 | 39015086432435 | A51C19 | Analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane / | 816702085 | 885059961 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432435; | ||||||||||||||||||
7 | NACARMBox001 | 39015086432740 | A51G31a | Summary of results of a wind-tunnel investigation of nine related horizontal tails / | 816702074 | 885133426 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432740 | ||||||||||||||||||
8 | NACARMBox004 | 39015086490292 | A51H10 | Lift, 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 / | 824989556 | 885132851 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086490292 | ||||||||||||||||||
9 | NACARMBox004 | 39015086489971 | A51H23 | Aerodynamic characteristics of a leading-edge slat on a 35 degree swept-back wing for Mach numbers from 0.30 to 0.88 / | 712649131 | 885133182 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086489971 | ||||||||||||||||||
10 | NACARMBox001 | 39015086432591 | A51L17a | Effect of various missile characteristics on airframe frequency response / | 816702086 | 885133413 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432591 | ||||||||||||||||||
11 | NACARMBox001 | 39015086432443 | A52A18 | Instrumentation of the ames supersonic free-flight wind tunnel / | 816701709 | 885133551 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432443 | ||||||||||||||||||
12 | NACARMBox001 | 39015086432757 | A52D01b | Boundary-layer measurements on several porous materials with suction applied / | 816702087 | 885146321 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432757 | ||||||||||||||||||
13 | NACARMBox001 | 39015086432609 | A52D24 | Supplementary note on modified-impact-theory calculations for bodies of revolution having minimum drag at hypersonic speeds / | 816702088 | 885133449 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432609 | ||||||||||||||||||
14 | NACARMBox001 | 39015086432450 | A52J08 | Downwash characteristics and vortex-sheet shape behind a 63 degree swept-back wing-fuselage combination at a Reynolds number of 6,100,000 / | 816690370 | 885198677 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432450 | ||||||||||||||||||
15 | NACARMBox001 | 39015086432765 | A53A30a | Effects 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 / | 816702071 | 885146315 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432765 | ||||||||||||||||||
16 | NACARMBox001 | 39015086432617 | A53E29 | Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds / | 816701705 | 885059870 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432617 | ||||||||||||||||||
17 | NACARMBox001 | 39015086432468 | A54A05 | Evaluation of two cooling-air ejectors in flight at transonic speeds / | 816701719 | 885060110 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432468 | ||||||||||||||||||
18 | NACARMBox001 | 39015086432773 | A54B18a | Investigation of a three-blade propeller in combination with two different spinners and an NACA D-type cowl at mach numbers up to 0.80 / | 816690384 | 885133396 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432773 | ||||||||||||||||||
19 | NACARMBox001 | 39015086432625 | A54F28 | On the range of applicability of the transonic area rule / | 130052568 | 857368937 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432625 | ||||||||||||||||||
20 | NACARMBox001 | 39015086432476 | A54H09 | Experimental and predicted longitudinal response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet / | 816690385 | 885133666 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432476 | ||||||||||||||||||
21 | NACARMBox005 | 39015086429787 | A54H23a | Investigation of the lift, center of pressure, and drag of a projectile at Mach number of 8.6 and a Reynolds number of 17 million / | 857063215 | 897078899 | Available HT 9/12/19, Search only in HT 1/17/2017 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086429787 | ||||||||||||||||||
22 | NACARMBox006 | 39015095100650 | A54K16 | Tracking performance of a swept-wing figher with a disturbed reticle lead-computing sight / | 968798376 | 1013869817 | Available HT 10/17/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015095100650 | ||||||||||||||||||
23 | NACARMBox001 | 39015086432484 | A55A18 | Wave drag of arbitrary configurations in linearized flow as determined by areas and forces in oblique planes / | 816690386 | 885060056 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432484 | ||||||||||||||||||
24 | NACARMBox001 | 39015086432633 | A55B07 | General theory of wave-drag reduction for combinations employing quasi-cylindrical bodies with an application to swept-wing and body combinations / | 816701704 | 885133438 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432633 | ||||||||||||||||||
25 | NACARMBox007 | 39015095338433 | A55B21 | Experimental investigation of two methods for reducing transonic drag of swept-wing and body combinations / | 1109543318 | |||||||||||||||||||||
26 | NACARMBox001 | 39015086432781 | A55C07 | Flight tests of a leading-edge area suction on a fighter-type airplane with a 35 degree sweptback wing / | 712654820 | 885060467 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432781 | ||||||||||||||||||
27 | NACARMBox007 | 39015095338250 | A55C08 | Correlation of airfoil section data with the aerodynamic loads measured on a 45 degree sweptback wing model at subsonic Mach numbers / | 1109593676 | |||||||||||||||||||||
28 | NACARMBox007 | 39015095338268 | A55D08 | 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 | NACARMBox007 | 39015095338276 | A55D11 | 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 | NACARMBox007 | 39015095338284 | A55D12 | Controls for supersonic missiles / | 1109533581 | |||||||||||||||||||||
31 | NACARMBox001 | 39015086432799 | A55D12a | Effects of powered controls and fire-control systems on tracking accuracy / | 816702090 | 885061023 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432799 | ||||||||||||||||||
32 | NACARMBox007 | 39015095338102 | A55D14 | Effects of flexibility on the longitudinal and lateral-directional response of a large airplane / | 694766832 | |||||||||||||||||||||
33 | NACARMBox007 | 39015095338110 | A55D27 | Experimental investigation at Mach numbers from 0 to 1.9 of trapezoidal and circular side inlets for a fighter-type airplane / | 1109696276 | |||||||||||||||||||||
34 | NACARMBox001 | 39015086432641 | A55D27a | Comparison 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 / | 816690387 | 885060451 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432641 | ||||||||||||||||||
35 | NACARMBox001 | 39015086432492 | A55E11a | Application of statistical theory to beam-rider guidance in the presence of noise. [Part] 2, Modified Wiener filter theory / | 712697852 | 885060413 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432492 | ||||||||||||||||||
36 | NACARMBox007 | 39015095338128 | A55E17 | Load distribution on wings and wing-body combinations at high angles of attack and supersonic speeds / | 1109543156 | |||||||||||||||||||||
37 | NACARMBox007 | 39015095338136 | A55E31 | Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 1.98 / | 712673762 | |||||||||||||||||||||
38 | NACARMBox007 | 39015095338144 | A55F02 | 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 | |||||||||||||||||||||
39 | NACARMBox007 | 39015095338151 | A55F15 | Drag and rolling-moment effectiveness of trailing-edge spoilers at Mach numbers 2.2 and 5.0 / | 1109555074 | |||||||||||||||||||||
40 | NACARMBox007 | 39015095338169 | A55F16 | Aerodynamic principles for the design of jet-engine induction systems / | 1264098695 | |||||||||||||||||||||
41 | NACARMBox007 | 39015095338292 | A55F21 | Flight investigation at transonic speeds of a model having a triangular wing of aspect ratio 2 / | 1109599127 | |||||||||||||||||||||
42 | NACARMBox001 | 39015086433243 | A55F21a | Discussion of methods for reducing aerodynamic heating in supersonic flight / | 66528800 | 885060482 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086433243 | ||||||||||||||||||
43 | NACARMBox007 | 39015095338300 | A55F23 | Preliminary experimental investigation of a variable-area, variable-internal-contraction air inlet at Mach numbers between 1.42 and 2.44 / | 1109713528 | |||||||||||||||||||||
44 | NACARMBox007 | 39015095338318 | A55F29 | Fuselage side inlets : a study of some factors affecting their performance and a comparison with nose inlets / | 1109638652 | |||||||||||||||||||||
45 | NACARMBox001 | 39015086432153 | A55G11 | Methods for connection to revolving thermocouples / | 816701741 | 885060814 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432153 | ||||||||||||||||||
46 | NACARMBox007 | 39015095338441 | A55H09 | 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 | NACARMBox007 | 39015095338458 | A55I15 | Method for simulating the atmospheric entry of long-range ballistic missiles / | 713021594 | |||||||||||||||||||||
48 | NACARMBox001 | 39015086432948 | A55J21 | Measurement of the longitudinal moment of inertia of a flexible airplane / | 713023096 | 885133700 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432948 | ||||||||||||||||||
49 | NACARMBox007 | 39015095338466 | A55J28 | Application of Tchebichef form of harmonic analysis to the calculation of zero-lift wave drag of wing-body-tail combinations / | 1109546779 | |||||||||||||||||||||
50 | NACARMBox007 | 39015095338474 | A55K07 | 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 | NACARMBox007 | 39015095338482 | A55K09 | Force, moment, and pressure-distribution characteristics of rectangular wings at high angles of attack and supersonic speeds / | 1109677894 | |||||||||||||||||||||
52 | NACARMBox001 | 39015086433235 | A55K10 | Influence of the body flow field on the zero-lift wave drag of wing-body combinations modified in accordance with the transonic area rule / | 816701732 | 885133325 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086433235 | ||||||||||||||||||
53 | NACARMBox007 | 39015095338490 | A55K21 | 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 | NACARMBox007 | 39015095338508 | A55L02 | 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 | NACARMBox007 | 39015095338326 | A55L05 | Aircraft configurations developing high lift-drag ratios at high supersonic speeds / | 133095291 | |||||||||||||||||||||
56 | NACARMBox001 | 39015086433086 | A55L13a | Heat-transfer characteristics of blunt two-and three-dimensional bodies at supersonic speeds / | 816702091 | 885060772 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086433086 | ||||||||||||||||||
57 | NACARMBox007 | 39015095338334 | A55L13b | Aerodynamics of missiles employing wings of very low aspect ratio / | 1109491117 | |||||||||||||||||||||
58 | NACARMBox007 | 39015095338342 | A55L13c | Aerodynamics of bodies, wings, and wing-body combinations at high angles of attack and supersonic speeds / | 1109590677 | |||||||||||||||||||||
59 | NACARMBox007 | 39015095338359 | A55L15 | Problems of performance and heating of hypersonic vehicles / | 694884782 | |||||||||||||||||||||
60 | NACARMBox007 | 39015095338177 | A55L16 | Study of a symmetrical, circular, internal compression inlet / | 1109633836 | |||||||||||||||||||||
61 | NACARMBox007 | 39015095338185 | A56B21 | Light diffusion through high-speed turbulent boundary layers / | 66528424 | |||||||||||||||||||||
62 | NACARMBox007 | 39015095338193 | A56B27 | 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 | NACARMBox007 | 39015095338201 | A56B27a | Method of reducing heat transfer to blunt bodies by air injection / | 713037714 | |||||||||||||||||||||
64 | NACARMBox007 | 39015095338219 | A56C01 | 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 | NACARMBox007 | 39015095338227 | A56C06 | Change with mass-flow ratio of the cowl pressure drag of normal-shock inlets at supersonic speeds / | 1109544981 | |||||||||||||||||||||
66 | NACARMBox007 | 39015095338235 | A56D23 | Use of area suction for improving the longitudinal characteristics of a thin unswept wing-fuselage model with leading- and trailing-edge flaps / | 713041927 | |||||||||||||||||||||
67 | NACARMBox007 | 39015095338243 | A56E24 | 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 | NACARMBox007 | 39015095338367 | A56F07 | Simulator study of some longitudinal stability and control problems of a piloted aircraft in flights to extreme altitude and high speed / | 1109549329 | |||||||||||||||||||||
69 | NACARMBox007 | 39015095338375 | A56F12 | Analysis of some parameters used in correlating blowing-type boundary-layer control data / | 713047402 | |||||||||||||||||||||
70 | NACARMBox007 | 39015095338383 | A56F15 | 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 | NACARMBox007 | 39015095338524 | A56G17 | Measurements of boundary-layer transition at low speed on two bodies of revolution in a low-turbulence wind tunnel / | 66528255 | |||||||||||||||||||||
72 | NACARMBox007 | 39015095338532 | A56G19 | 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 | NACARMBox007 | 39015095338516 | A56G30 | 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 | NACARMBox007 | 39015095338540 | A56H06 | 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 | NACARMBox007 | 39015095337658 | A56H08 | 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 | NACARMBox007 | 39015095337666 | A56H27 | 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 | NACARMBox005 | 39015086429795 | A56H31 | Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4 / | 713270945 | 897078906 | Available HT 10/17/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086429795 | ||||||||||||||||||
78 | NACARMBox007 | 39015095337674 | A56I05 | Some experiments at high supersonic speeds on the aerodynamic and boundary-layer transition characteristics of high-drag bodies of revolution / | 1109623770 | |||||||||||||||||||||
79 | NACARMBox007 | 39015095337807 | A56L18 | Effects of conical camber on the lift, drag, and pitching-moment characteristics of a triangular wing of aspect ratio 3.0 / | 713295706 | |||||||||||||||||||||
80 | NACARMBox007 | 39015095337815 | A57A02 | Investigation of wing-body juncture interference effects at transonic speeds for several swept-wing and body combinations / | 713316385 | |||||||||||||||||||||
81 | NACARMBox007 | 39015095337823 | A57A24 | 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 | NACARMBox007 | 39015095337955 | A57A25 | Lateral-directional aerodynamic characteristics of several coplanar triple-body missile configurations at Mach numbers from 0.6 to 1.4 / | 1109543986 | |||||||||||||||||||||
83 | NACARMBox007 | 39015095337963 | A57B11 | Leading-edge contours for thin swept wings : an analysis of low-and high-speed data / | 713314618 | |||||||||||||||||||||
84 | NACARMBox007 | 39015095337971 | A57B14 | 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 | NACARMBox007 | 39015095337682 | A57C19 | Air-borne target simulator for use with scope-presentation type fire-control systems / | 1264098696 | |||||||||||||||||||||
86 | NACARMBox007 | 39015095337831 | A57C25 | Investigation of boundary-layer transition on flat-faced bodies of revolution at high supersonic speeds / | 1109533358 | |||||||||||||||||||||
87 | NACARMBox007 | 39015095337989 | A57D04 | Analytical study of the comparative pitch-up behavior of several airplanes and correlation with pilot opinion / | 713322582 | |||||||||||||||||||||
88 | NACARMBox007 | 39015095337690 | A57D09 | Flight tests of an automatic interceptor system with a tracking radar modified to minimize the interaction between antenna and interceptor motions / | 1109574413 | |||||||||||||||||||||
89 | NACARMBox007 | 39015095337849 | A57D11 | 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 | NACARMBox007 | 39015095337997 | A57D30 | Comparison of carrier approach speeds as determined from flight tests and from pilot-operated simulator studies / | 713322734 | |||||||||||||||||||||
91 | NACARMBox007 | 39015095337708 | A57E21 | Aerodynamic loads on tails at high angles and sideslip / | 1109692681 | |||||||||||||||||||||
92 | NACARMBox007 | 39015095337856 | A57E24 | Investigation of axially symmetric flow over steps at transonic speeds with comparisons of estimated and experimental drag results / | 713329068 | |||||||||||||||||||||
93 | NACARMBox001 | 39015086432930 | A57F03a | Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds / | 816690388 | 885060933 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086432930 | ||||||||||||||||||
94 | NACARMBox001 | 39015086433227 | A57F06a | A 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 / | 713325058 | 885060498 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086433227 | ||||||||||||||||||
95 | NACARMBox005 | 39015086429803 | A57F06b | Effects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4 / | 713342092 | 897078907 | Available HT 10/17/2019, | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086429803 | ||||||||||||||||||
96 | NACARMBox007 | 39015095338003 | A57F26 | Effects of target and missile characteristics on theoretical minimum miss distance for a beam-rider guidance system in the presence of noise / | 459552600 | |||||||||||||||||||||
97 | NACARMBox007 | 39015095337716 | A57G10 | 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 | NACARMBox007 | 39015095338391 | A57G16 | Wing-body combinations with wings of very low aspect ratio at supersonic speeds / | 1109542578 | |||||||||||||||||||||
99 | NACARMBox007 | 39015095337864 | A57H19 | 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 | NACARMBox001 | 39015086433078 | A57H19a | Transonic investigation of the effects of semisubmerged-store cavities and of slots on the zero-lift drag of a body of revolution / | 816701733 | 885060672 | Available HT 10/17/2019, NOT IN HT 1/13/2014 | https://babel.hathitrust.org/cgi/pt?id=mdp.39015086433078 | ||||||||||||||||||
101 | NACARMBox007 | 39015095338011 | A57H21 | 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 |