732 Matching Results

Search Results

Results: 1 - 24 next
Primary view of Tables of Chemical Kinetics : Homogeneous Reactions (Supplementary Tables)
United States. Bureau of Standards.
September 15, 1961
Primary view of Microwave Spectral Tables: [Volume 2.] Line Strengths of Asymmetric Rotors
Wacker, Paul F. & Pratto, Marlene R.
December 15, 1964
Primary view of Standard Cells: Their Construction, Maintenance, and Characteristics
Hamer, Walter J.
January 15, 1965
Primary view of The HASL Surface Air Sampling Program Summary Report For 1963
Volchok, Herbert L. (Herbert Lee), 1926-1987
January 15, 1965
Primary view of Realistic Uncertainties and the Mass Measurement Process: An Illustrated Review
Pontius, P. E. & Cameron, J. M.
August 15, 1967
Primary view of Galveston Area (ARMS-II)
Guillou, R. B.
January 15, 1963
Primary view of Preliminary Design Requirements Argonne Boiling Reactor (ARBOR) Facility
Fromm, L. W.; Bernsen, S. A.; Bullinger, C. F. & Matousek, J. F.
July 15, 1957
Primary view of Electronic Devices for Nuclear Physics: February 1, 1956 - April 30, 1956
Greenblatt, M. H.; Matheson, R. M.; Sommer, A. H.; Fowler, G. O. & Spicer, W. E.
June 15, 1956
Primary view of Experimental Investigation of Diffuser Pressure Ratio Control With Shock Positioning Limit on 28 Inch Ram-Jet Engine
Dunbar, William R.; Wentworth, Carl B. & Crowl, Robert J.
January 15, 1957
Primary view of A Study of Injection Processes for 15-percent Fluorine-85- Percent Oxygen and Heptane in a 200-pound-thrust Rocket Engine
Heidmann, M. F.
January 15, 1957
Primary view of Transonic Flutter Investigation of Models of the Sweptback Wing of a Fighter Airplane
Smith, Samuel L., III & Boswinkle, Robert W., Jr.
April 15, 1958
Primary view of Preliminary Wind-Tunnel Investigation of the Performance of Republic F-105 Wing-Root Inlet Configurations at Various Angles of Attack and a Mach Number of 2.01
Kouyoumjian, Walter L.
January 15, 1957
Primary view of Effects of Components and Various Modifications on the Drag and the Static Stability and Control Characteristics of a 42 Deg Swept-Wing Fighter-Airplane Model at Mach Numbers of 1.60 to 2.50
Church, James D.
April 15, 1959
Primary view of Preliminary Free-Jet Performance of XRJ43-MA-3 Ram-Jet Engine at a Mach Number of 2.70
Welna, Henry J. & Campbell, Carl E.
April 15, 1955
Primary view of Altitude Performance of a 20-Inch-Diameter Ram-Jet Engine Investigated in a Free-Jet Facility at Mach Number 3.0
Smolak, George R. & Wentworth, Carl B.
June 15, 1953
Primary view of Experimental Investigation of Laminar-Boundary-Layer Control on an Airfoil Section Equipped With Suction Slots Located at Discontinuities in the Surface Pressure Distribution
Loftin, Laurence K., Jr. & Horton, Elmer A.
December 15, 1953
Primary view of Effect of Ice Formations on Section Drag of Swept NACA 63A-009 Airfoil with Partial-Span Leading-Edge Slat for Various Modes of Thermal Ice Protection
von Glahn, Uwe H. & Gray, Vernon H.
March 15, 1954
Primary view of Preliminary Investigation of a Technique for Stability Studies of a Self-Propelled Model of a Submerged Submarine
McKann, Robert E. & Petynia, William W.
April 15, 1954
Primary view of Altitude Free-Jet Investigation of Dynamics of a 28-Inch-Diameter Ram-Jet Engine
Wentworth, Carl B.; Dunbar, William R. & Crowl, Robert J.
January 15, 1957
Primary view of Relation of Turbojet Propulsion System Development to the Strategic Bomber Mission
Rothrock, Addison M.; Cesaro, Richard S. & Walker, Curtis L.
August 15, 1956
Primary view of Preliminary Transonic Flutter Investigation of Models of T-Tall of Blackburn NA-39 Airplane
Jones, George W., Jr. & Boswinkle, Robert W., Jr.
April 15, 1958
Primary view of Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured in Flight on the Wing of the Douglas D-558-I Airplane for a 1 g Stall, a Speed Run to a Mach Number of 0.90, and a Wind-Up Turn at a Mach Number of 0.86
Keener, Earl R. & Pierce, Mary
December 15, 1950
Primary view of Some Transonic Aerodynamic Characteristics of a Model Similar to the McDonnell F3H-2N Airplane
Crabill, Norman L. & Jackson, Bruce G.
May 15, 1956
Primary view of Zero-Lift Drag of the Chance Vought Regulus II Missile at Mach Numbers Between 0.8 and 2.2 as Determined From the Flight Tests of Two 0.12-Scale Models
Church, James D.
July 15, 1954
Back to Top of Screen