National Advisory Committee for Aeronautics (NACA) - Browse

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Primary view of Wind-tunnel Tests of the Static Longitudinal Characteristics at Low Speed of a Swept-wing Airplane With Blowing Flaps and Leading-edge Slats
James, H. A. & Maki, R. L.
April 5, 1957
Primary view of Wing-body combinations with wings of very low aspect ratio at supersonic speeds
Jorgensen, L. H. & Katzen, E. D.
October 26, 1956
Primary view of Boundary-layer-transition measurements in full-scale flight
Banner, R. D.; Mctigue, J. G. & Petty, G., 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 Altitude performance of a 20-inch-diameter ram-jet engine investigated in a free-jet facility at Mach number 3.0
Smolak, G. R. & Wentworth, C. B.
June 15, 1953
Primary view of Comparison and evaluation of two model techniques used in predicting bomb-release motions
Carlson, H. W.; Geier, D. J. & Lee, J. B.
December 27, 1957
Primary view of Pressure Distributions and Aerodynamic Characteristics of Several Spoiler-type Controls on a Trapezoidal Wing at Mach Numbers of 1.61 and 2.01
Czarnecki, K. R. & Lord, D. R.
July 26, 1956
Primary view of Aerodynamic characteristics of a 0.04956-scale model of the Convair F-102A airplane at Mach numbers of 1.41, 1.61, and 2.01
Spearman, M. Leroy & Driver, Cornelius
September 30, 1955
Primary view of Transonic flight evaluation of the effects of fuselage extension and indentation on the drag of a 60 deg delta wing interceptor airplane
Asher, W. P. & Saltzman, E. J.
September 26, 1957
Primary view of Analysis of flight-determined and predicted effects of flexibility on the steady-state wing loads of the B-52 airplane
Kuhl, A. E.; Little, M. V. & Rogers, J. T.
April 23, 1958
Primary view of Induction system characteristics and engine surge occurrence for two fighter-type airplanes
Bellman, D. R.; Larson, T. J. & Thomas, G. M.
May 26, 1958
Primary view of In-flight Gains Realized by Modifying a Twin Side-inlet Induction System
Saltzman, E. J.
December 12, 1957
Primary view of Power-off tests of the Northrop N9M-2 tailless airplane in the 40- by 80-foot wind tunnel
Stevens, Victor I., Jr. & Mccormack, Gerald M.
December 14, 1944
Primary view of Heat Transfer Measured in Free Flight on a Slightly Blunted 25 deg Cone-Cylinder-Flare Configuration at Mach Numbers up to 9.89
Bond, Aleck C.; Lee, Dorothy B. & Rumsey, Charles B.
September 26, 1958
Primary view of Model ditching investigations of three airplanes equipped with hydro-skis
Fisher, L. J.
April 25, 1950
Primary view of A note on the ability to predict transonic drag-rise changes due to model modifications
Pierpont, P. K.
October 3, 1957
Primary view of The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-fuselage-store Configurations. Ii - Swept-wing Heavy-bomber Configuration With Large Store Nacelle . Lateral Forces and Pitching Moments, Mach Number, 1.61
Carlson, H. W. & Smith, N. F.
July 6, 1955
Primary view of Aerodynamic heating of blunt nose shapes at Mach numbers up to 14
Stoney, W. E., Jr.
August 11, 1958
Primary view of The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-fuselagestore Configurations. 1.-swept-wing Heavy-bomber Configuration With Large Store Nacelle . Lift and Drag, Mach Number, 1.61
Carlson, H. W. & Smith, N. F.
March 11, 1955
Primary view of The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-fuselagestore Configurations. Iii - Swept-wing Fighter-bomber Configuration With Large and Small Stores. Mach Number, 1.61
Carlson, H. W. & Smith, N. F.
September 15, 1955
Primary view of Aerodynamics of Oscillating Control Surfaces at Transonic Speeds
Clevenson, S. A. & Thompson, R. F.
June 17, 1957
Primary view of Aerodynamic loads on an external store adjacent to a 60 deg delta wing at mach numbers from 0.75 to 1.96
Hadaway, W. M.
April 24, 1956
Primary view of Aerodynamic Loads on an External Store Adjacent to an Unswept Wing at Mach Numbers Between 0.75 and 1.96
Hadaway, W. M.
February 17, 1956
Primary view of Aeronautical Lab. Examination of Recent Lateral-stability-derivative Data
Kuhn, R. F. & Malvestuto, F. S., Jr.
October 22, 1953