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Collection
National Advisory Committee for Aeronautics Collection
1,100
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National Advisory Committee for Aeronautics Collection
1,100
Technical Report Archive and Image Library
1,100
Serial/Series Title
NACA Research Memorandums
424
NACA Technical Notes
375
NACA Technical Memorandums
121
NACA Wartime Reports
106
NACA Technical Reports
48
NACA Advanced Restricted Reports
37
NACA Memorandum Reports
31
NACA Advanced Confidential Reports
30
NACA Aircraft Circulars
17
NACA Restricted Bulletins
8
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NACA Research Memorandums
424
NACA Technical Notes
375
NACA Technical Memorandums
121
NACA Wartime Reports
106
NACA Technical Reports
48
NACA Advanced Restricted Reports
37
NACA Memorandum Reports
31
NACA Advanced Confidential Reports
30
NACA Aircraft Circulars
17
NACA Restricted Bulletins
8
NACA Special Reports
7
NACA Confidential Bulletins
2
Technical note (United States. National Advisory Committee for Aeronautics)
2
NACA Research Memorandum
1
Decade
1960-1969
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1950-1959
557
1940-1949
366
1930-1939
91
1920-1929
85
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1960-1969
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1940-1949
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91
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1964
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1958
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1957
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1956
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1955
65
1954
42
1953
56
1952
67
1951
60
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1958
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1953
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1950
51
1949
30
1948
75
1947
81
1946
34
1945
32
1944
24
1943
29
1942
33
1941
16
1940
12
1939
10
1938
10
1937
7
1936
9
1935
5
1934
9
1933
9
1932
12
1931
10
1930
10
1929
8
1928
12
1927
9
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1920
4
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July
1,100
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July
1,100
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National Advisory Committee for Aeronautics Collection
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Spin-Tunnel Investigation of a 1/28-Scale Model of a Subsonic Attack Airplane
Some Research on the Lift and Stability of Wing-Body Combinations
Experimental Investigation of Flutter and Divergence Characteristics of the Rocket-Motor Fin of the ASROC Missile
Experimental investigation of flutter and divergence characteristics of the rocket-motor fin of the ASROC missile: COORD. No. N-AM-66
Altitude Performance of the Afterburner on the Iroquois Turbojet Engine. Coord. No. AF-P-6
Boundary-Layer-Transition Measurements in Full-Scale Flight
Boundary-Layer-Transition Measurements in Full-Scale Flight
Chemical and physical factors affecting combustion in fuel-nitric acid systems
Evaluation of Three Injectors in a 2400-Pound-Thrust Rocket Engine Using Liquid Oxygen and Liquid Ammonia
Investigation of a Prototype Iroquois Turbojet Engine in an Altitude Test Chamber Coord. No. AF-P-6
An Investigation of the Effect of Target Temperature on Projectile Penetration and Cratering
An Investigation of the Effect of Target Temperature on Projectile Penetration and Cratering
Turbulent Skin Friction at High Mach Numbers and Reynolds Numbers
Free-Spinning-Tunnel Investigation of a 1/28-Scale Model of the North American FJ-4 Airplane with External Fuel Tanks, TED No. NACA AD 3112
The Effect of Compressor-Inlet Water Injection on Engine and Afterburner Performance
The Effect of Compressor-Inlet Water Injection on Engine and Afterburner Performance
Effect of Design Variables on Performance of Mach 4.0 Hydrogen Expansion Engines
Effect of Design Variables on Performance of Mach 4.0 Hydrogen Expansion Engines
Performance of Five Short Multielement Turbojet Combustors for Hydrogen Fuel in Quarter-Annulus Duct
Performance of five short multielement turbojet combustors for hydrogen fuel in quarter-annulus duct
Effects of Wing Sweep, Horizontal-Tail Configuration, and a Ventral Fin on Static Stability Characteristics of a Model With a Wing of Aspect Ratio 3 at Mach Numbers From 2.29 to 4.65
Investigation of the aerodynamic characteristics of a model of a supersonic bomber configuration with a swept and an unswept wing at Mach numbers from 1.79 to 2.67
Operational problems of manned orbital vehicles
Preliminary Aerodynamic Data Pertinent to Manned Satellite Reentry Configurations
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