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Primary view of 100 Areas engineers technical activities report, December 1950
unknown creator
January 2, 1951
Primary view of 100 areas technical activities report engineers, February, 1951
unknown creator
March 1, 1951
Primary view of 100 Areas technical activities report Engineers, January 1951
unknown creator
February 2, 1951
Primary view of 100 Areas technical activities report, engineers - March 1951
unknown creator
April 1, 1951
Primary view of 100 Areas technical activities report - physics, July 1951
unknown creator
August 3, 1951
Primary view of 100 Areas technical activities report -- Physics, November 1951
unknown creator
December 6, 1951
Primary view of 300-KV Pulser Transformer and Pulser.
Heller, R. E.
November 1951
Primary view of Acenaphthene solvents for use in Building 313 Frost Test operation
Kratzer, W. K.
June 26, 1951
Primary view of Acid-Mine-Drainage Problems: Anthracite Region of Pennsylvania
Ash, S. H. (Simon Harry), b. 1889; Felegy, E. W.; Kennedy, D. O. & Miller, P. S.
1951
Primary view of The Action of Oxygen on Activated Charcoal
Bigelow, J. E.; Belaga, M. W. & Mulvihill, R. J.
June 29, 1951
Primary view of Adaptation of a Cascade Impactor to Flight Measurement of Droplet Size in Clouds
Levine, Joseph & Kleinknecht, Kenneth S.
September 18, 1951
Primary view of Addition of standard quantities of chemicals in certain reduction operations in the 234-5 Building
Desposato, F.E.
September 28, 1951
Primary view of ADDITIONAL PULSE COLUMN TESTS FOR URANIUM ORES RECOVERY PROCESS
Jealous, A.C.
June 29, 1951
Primary view of Additional Studies of the Stability and Controllability of an Unswept-Wing Vertically Rising Airplane Model in Hovering Flight Including Studies of Various Tethered Landing Techniques
Bates, William R.; Lovell, Powell M., Jr. & Smith, Charles C., Jr.
November 6, 1951
Primary view of The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow
Chang, Chieh-Chien
October 1951
Primary view of Aerodynamic characteristics at transonic speeds of a 69 degree delta wing with a triangular plan-form control having a skewed hinge axis and an overhang balance: transonic-bump method
Wiley, Harleth G.
February 6, 1951
Primary view of Aerodynamic characteristics including pressure distribution of a fuselage and three combinations of the fuselage with swept-back wings at high subsonic speeds
Sutton, Fred B. & Martin, Andrew
February 6, 1951
Primary view of Aerodynamic Characteristics of a Flying-Boat Hull Having a Length-Beam Ratio of 15, TED No. NACA 2206
Riebe, John M. & Naeseth, Rodger L.
January 23, 1951
Primary view of Aerodynamic characteristics of a slender cone-cylinder body of revolution at a Mach number of 3.85
Jack, John R.
November 5, 1951
Primary view of Aerodynamic Characteristics of Bodies at Supersonic Speeds: A Collection of Three Papers
Seiff, Alvin; Sandahl, Carl A.; Chapman, Dean R.; Perkins, E. W. & Gowen, F. E.
November 9, 1951
Primary view of Aerodynamic Characteristics of Four Bodies of Revolution Showing Some Effects of Afterbody Shape and Fineness Ratio at Free-Stream Mach Numbers From 1.50 to 1.99
Cohen, Robert J.
May 22, 1951
Primary view of Aerodynamic Characteristics of Four Wings of Sweepback Angles 0 Degrees, 35 Degrees, 45 Degrees, and 60 Degrees, NACA 65A006 Airfoil Section, Aspect Ratio 4, and Taper Ratio 0.6 in Combination With a Fuselage at High Subsonic Mach Numbers and at a Mach Number of 1.2
Luoma, Arvo A.
June 6, 1951
Primary view of Aerodynamic Characteristics of Tapered Wings Having Aspect Ratios of 4, 6, and 8, Quarter-Chord Lines Swept Back 45 Degrees, and NACA 63(Sub 1)a012 Airfoil Sections: Transonic-Bump Method
Polhamus, Edward C. & King, Thomas J., Jr.
June 13, 1951
Primary view of Aerodynamic characteristics of the NACA RM-10 research missile in the Ames 1- by 3-foot supersonic wind tunnel no. 2: Pressure and force measurements at Mach numbers of 1.52 and 1.98
Perkins, Edward W.; Gowen, Forrest E. & Jorgensen, Leland H.
September 19, 1951
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