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Primary view of Aerodynamic Characteristics of a 0.5-Scale Model of the Fairchild XSAM-N-2 Lark Missile at High Subsonic Speeds
Martin, Andrew & Hunter, Harlo A.
September 28, 1949
Primary view of Aerodynamic Characteristics of Two All-Movable Wings Tested in the Presence of a Fuselage at a Mach Number of 1.9
Conner, D. William
October 28, 1948
Primary view of Aerodynamic characteristics of two rectangular-plan-form, all moveable controls in combination with a slender body of revolution at Mach numbers from 3.00 to 6.25
Wong, Thomas J. & Gloria, Hermilo R.
December 28, 1955
Primary view of Aerodynamic Characteristics of Two Rectangular-plan-form, Allmovable Controls in Combination With a Slender Body of Revolution at Mach Numbers From 3.00 to 6.25
Wong, Thomas J. & Gloria, Hermilo R.
December 28, 1955
Primary view of Aerodynamic Characteristics of Wings Designed for Structural Improvement
Weil, Joseph & Polhamus, Edward C.
May 28, 1951
Primary view of Aerodynamic Loading Characteristics in Sideslip of a 45 Degree Sweptback Wing With and Without a Fence at High Subsonic Speeds
Kuhn, Richard E.
January 28, 1955
Primary view of Aeronautical interference effects on normal and axial force coefficients of several engine-strut-body configurations at Mach numbers of 1.8 and 2.0
Kremzier, Emil J. & Dryer, Murray
April 28, 1952
Primary view of Altitude performance and operational characteristics of 29-inch-diameter tail-pipe burner with several fuel systems and fuel-cooled stage-type flame holders on J35-A-5 turbojet engine
Golladay, Richard L. & Bloomer, Harry E.
April 28, 1950
Primary view of Altitude performance of a full-scale turbojet engine using pentaborane fuels
Useller, James W.; Kaufman, Warner B. & Jones, William L.
February 28, 1957
Primary view of Altitude performance of J71-A-2(600-D1) turbojet engine
Smith, Ivan D. & Sivo, Joseph N.
December 28, 1956
Primary view of Altitude Performance of the Afterburner on the Iroquois Turbojet Engine. Coord. No. AF-P-6
Groesbeck, Donald E. & Peters, Daniel J.
July 28, 1958
Primary view of Altitude-Wind-Tunnel Investigation of R-4360-18 Power-Plant Installation for XR60 Airplane, 3, Performance of Induction and Exhaust Systems
Dupree, David T. & Hawkins, W. Kent
March 28, 1947
Primary view of Analysis of a Pressure-Jet Power Plant for Helicopter
Krebs, Richard P. & Miller, William S., Jr.
March 28, 1955
Primary view of An Analysis of the Full-Floating Journal Bearing
Shaw, M. C. & Nussdorfer, T. J., Jr.
January 28, 1947
Primary view of Analytical investigation of off-design performance of a transonic turbine
Whitney, Warren J. & Stewart, Warner L.
May 28, 1954
Primary view of Application of wing-body theory to drag reduction at low supersonic speeds
Baldwin, Barrett S., Jr. & Dickey, Robert R.
January 28, 1955
Primary view of Attenuation of Tangential-Pressure Oscillations in a Liquid-Oxygen-n-Heptane Rocket Engine With Longitudinal Fins
Priem, Richard J.
June 28, 1956
Primary view of Attenuation of tangential-pressure oscillations in a liquid-oxygen - n-heptane rocket engine with longitudinal fins
Priem, Richard J.
June 28, 1956
Primary view of A Bibliography of NACA Reports on Control of Turbojet Engines
Sanders, John C.
June 28, 1956
Primary view of Boundary-Layer-Transition Measurements in Full-Scale Flight
Banner, Richard D.; McTigue, John G. & Petty, Gilbert, Jr.
July 28, 1958
Primary view of Boundary-Layer-Transition Measurements in Full-Scale Flight
Banner, Richard D.; McTigue, John G. & Petty, Gilbert, Jr.
July 28, 1958
Primary view of Chemical and physical factors affecting combustion in fuel-nitric acid systems
Baker, Louis, Jr.
July 28, 1958
Primary view of Combustion properties of aluminum as ram-jet fuel
Branstetter, J. Robert; Lord, Albert M. & Gerstein, Melvin
March 28, 1951
Primary view of Comparison of High-Speed Operating Characteristics of Size 215 Cylindrical-Roller Bearings as Determined in Turbojet Engine and in Laboratory Test Rig
Macks, E. Fred & Nemeth, Zolton N.
November 28, 1951
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