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Primary view of The 6-Foot-4-Inch Wind Tunnel at the Washington Navy Yard
Desmond, G. L. & McCrary, J. A.
August 1935
Primary view of Absorbing landing shocks
Warner, Edward P.
August 1923
Primary view of Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics 3: effect of turbine stator adjustment
Rohlik, Harold E. & Rebeske, John J.
August 2, 1954
Primary view of Accelerations and passenger harness loads measured in full-scale light-airplane crashes
Eiband, A. Martin; Simpkinson, Scott H. & Black, Dugald O.
August 1953
Primary view of Accelerations Measured at Center of Gravity and Along Span of the Wing of a B-24D Airplane in Landing Impacts
Westfall, John R.
August 1944
Primary view of Accuracy of Approximate Methods for Predicting Pressures on Pointed Nonlifting Bodies of Revolution in Supersonic Flow
Ehret, Dorris M.
August 1952
Primary view of Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces
Krishnamurty, K.
August 1955
Primary view of Additional comparisons between computed and measured transonic drag-rise coefficients at zero lift for wing-body-tail configurations
Holdaway, George H.
August 15, 1955
Primary view of 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
Spreeman, Kenneth P. & Few, Albert G., Jr.
August 10, 1954
Primary view of Additional Test Data on Static Longitudinal Stability
Hübner, Walter
August 1934
Primary view of Adhesion of Ice in Its Relation to the De-Icing of Airplanes
Rothrick, A. M. & Selden, R. F.
August 1939
Primary view of 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
Robinson, Ross B. & Bernot, Peter T.
August 4, 1958
Primary view of 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
Robinson, Ross B. & Bernot, Peter T.
August 4, 1958
Primary view of 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
Spearman, M. Leroy & Robinson, Ross B.
August 30, 1954
Primary view of 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
Hallissy, Joseph M., Jr. & Hasson, Dennis F.
August 4, 1958
Primary view of 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
Hamilton, Clyde V.
August 1, 1952
Primary view of 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
Kuhn, Richard E. & Draper, John W.
August 18, 1953
Primary view of Aerodynamic Characteristics of a 45 Degree Swept-Back Wing With Aspect Ratio of 3.5 and NACA 2S-50(05)-50(05) Airfoil Sections
Proterra, Anthony J.
August 4, 1947
Primary view of Aerodynamic characteristics of a two-blade NACA 10-(3)(12)-03 propeller
Allis, A. E. & Gray, W. H.
August 30, 1948
Primary view of The aerodynamic characteristics of an aspect-ratio-20 wing having thick airfoil sections and employing boundary-layer control by suction
Cocke, Bennie W., Jr.; Fink, Marvin P. & Gottlieb, Stanley M.
August 1953
Primary view of Aerodynamic Characteristics of Several Airfoils of Low Aspect Ratio
Zimmerman, C. H.
August 1935
Primary view of Aerodynamic characteristics of several tip controls on a 60 degree wing at a Mach number of 1.61
Lord, Douglas R. & Czarnecki, K. R.
August 5, 1954
Primary view of 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)
Loftin, Laurence K., Jr.
August 1954
Primary view of Aerodynamic Characteristics of Three Deep-Step Planing-Tail Flying-Boat Hulls and a Transverse-Step Hull with Extended Afterbody
Riebe, John M. & Naeseth, Rodger L.
August 1952
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