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National Advisory Committee for Aeronautics Collection
1,158
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National Advisory Committee for Aeronautics Collection
1,158
Technical Report Archive and Image Library
1,158
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NACA Research Memorandums
469
NACA Technical Notes
339
NACA Technical Memorandums
119
NACA Wartime Reports
118
NACA Technical Reports
77
NACA Advanced Restricted Reports
45
NACA Memorandum Reports
41
NACA Aircraft Circulars
23
NACA Advanced Confidential Reports
18
NACA Special Reports
13
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NACA Research Memorandums
469
NACA Technical Notes
339
NACA Technical Memorandums
119
NACA Wartime Reports
118
NACA Technical Reports
77
NACA Advanced Restricted Reports
45
NACA Memorandum Reports
41
NACA Aircraft Circulars
23
NACA Advanced Confidential Reports
18
NACA Special Reports
13
NACA Restricted Bulletins
11
NACA Collection Reports
1
Technical note (United States. National Advisory Committee for Aeronautics)
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Accomack County, VA
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Cuyahoga County, OH
2
Accomack County, VA
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1950-1959
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366
1930-1939
107
1920-1929
99
1910-1919
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1950-1959
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1958
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80
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55
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22
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42
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24
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7
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1920
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August
1,158
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August
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National Advisory Committee for Aeronautics Collection
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The 6-Foot-4-Inch Wind Tunnel at the Washington Navy Yard
Absorbing landing shocks
Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics 3: effect of turbine stator adjustment
Accelerations and passenger harness loads measured in full-scale light-airplane crashes
Accelerations Measured at Center of Gravity and Along Span of the Wing of a B-24D Airplane in Landing Impacts
Accuracy of Approximate Methods for Predicting Pressures on Pointed Nonlifting Bodies of Revolution in Supersonic Flow
Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces
Additional comparisons between computed and measured transonic drag-rise coefficients at zero lift for wing-body-tail configurations
Additional Results on the Static Longitudinal and Lateral Stability Characteristics of a 0.05-Scale Model of the Convair F2Y-1 Airplane at High Subsonic Speeds
Additional Test Data on Static Longitudinal Stability
Adhesion of Ice in Its Relation to the De-Icing of Airplanes
Aerodynamic Characteristics at a Mach Number of 6.8 of Two Hypersonic Missile Configurations, One With Low-Aspect-Ratio Cruciform Fins and Trailing-Edge Flaps and One With a Flared Afterbody and All-Movable Controls
Aerodynamic Characteristics at a Mach Number of 6.8 of Two Hypersonic Missile Configurations, One With Low-Aspect-Ratio Cruciform Fins and Trailing-Edge Flaps and One With a Flared Afterbody and All-Movable Controls
Aerodynamic characteristics at Mach number of 2.01 of two cruciform missile configurations having 70 degree delta wings with length-diameter ratios of 14.8 and 17.7 with several canard controls
Aerodynamic characteristics at Mach numbers 2.36 and 2.87 of an airplane configuration having a cambered arrow wing with a 75 degree swept leading edge
Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2: Effects of sweep angle and thickness ratio on the static lateral stability characteristics at M = 2.01
Aerodynamic Characteristics in Pitch and Sideslip at High Subsonic Speeds of a 1/14-Scale Model of the Grumman XF104 Airplane with Wing Sweepback of 42.5 Degrees
Aerodynamic Characteristics of a 45 Degree Swept-Back Wing With Aspect Ratio of 3.5 and NACA 2S-50(05)-50(05) Airfoil Sections
Aerodynamic characteristics of a two-blade NACA 10-(3)(12)-03 propeller
The aerodynamic characteristics of an aspect-ratio-20 wing having thick airfoil sections and employing boundary-layer control by suction
Aerodynamic Characteristics of Several Airfoils of Low Aspect Ratio
Aerodynamic characteristics of several tip controls on a 60 degree wing at a Mach number of 1.61
Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10(exp. 6) to 8.0 x 10(exp. 6)
Aerodynamic Characteristics of Three Deep-Step Planing-Tail Flying-Boat Hulls and a Transverse-Step Hull with Extended Afterbody
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