National Advisory Committee for Aeronautics (NACA) - 4,160 Matching Results

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Primary view of Critical combinations of shear and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation
Batdorf, S. B. & Houbolt, John C.
January 1945
Primary view of NACA Mach number indicator for use in high-speed tunnels
Smith, Norman F.
July 1943
Primary view of Profile-Drag Coefficients of Conventional and Low-Drag Airfoils as Obtained in Flight
Zalovcik, John A.
May 1944
Primary view of On a New Method for Calculating the Potential Flow Past a Body of Revolution
Kaplan, Carl
July 1942
Primary view of Ditching Tests With 1/10-Size Model of the Army a-20a Airplane 1: Calm-Water Tests in NACA Tank No.2
Dawson, John R. & Jarvis, George A.
November 1943
Primary view of The development and application of high-critical-speed nose inlets
Baals, Donald D.; Smith, Norman F. & Wright, John B.
July 1945
Primary view of An Experimental Investigation of Rectangular Exhaust-Gas Ejectors Applicable for Engine Cooling
Manganiello, Eugene J. & Bogatsky, Donald
May 1945
Primary view of Wind-Tunnel Investigation of the Effects of Spoilers on the Characteristics of a Low-Drag Airfoil Equipped With a 0.25-Chord Slotted Flap
Holtzclaw, Ralph W.
July 23, 1945
Primary view of An Investigation of a Thermal Ice-Prevention System for a C-46 Cargo Airplane 5: Effect of Thermal System on Airplane Cruise Performance
Selna, James
May 1945
Primary view of On the Flow of a Compressible Fluid by the Hodography Method 1: Unification and Extension of Present-Day Results
Garrick, I. E. & Kaplan, Carl
March 1944
Primary view of A Concise Theoretical Method for Profile-Drag Calculation; Advance Report
Nitzberg, Gerald E.
February 1944
Primary view of An Investigation of a Thermal Ice-Prevention System for a C-46 Cargo Airplane 3: Description of Thermal Ice-Prevention Equipment for Wings, Empennage, and Windshield
Jones, Alun R. & Spies, Ray J., Jr.
February 1945
Primary view of The Lagrangian Multiplier Method of Finding Upper and Lower Limits to Critical Stresses of Clamped Plates
Budiansky, Bernard & Hu, Pai C.
1946
Primary view of Flight Measurements of the Effect of Various Amounts of Aileron Droop on the Low-Speed Lateral-Control Characteristics of an Observation Airplane
Turner, William N.
August 18, 1943
Primary view of An Investigation of a Thermal Ice-Prevention System for a C-46 Cargo Airplane 4: Results of Flight Tests in Dry-Air and Natural-Icing Conditions
Selna, James; Neel, Carr B., Jr. & Zeiller, E. Lewis
February 1945
Primary view of Determination of General Relations for the Behavior of Turbulent Boundary Layers
von Doenhoff, Albert E. & Tetervin, Neal
July 1943
Primary view of Analysis of Heat and Compressibility Effects in Internal Flow Systems and High-Speed Tests of a Ram-Jet System
Becker, John V. & Baals, Donald D.
September 1942
Primary view of Flight Studies of the Horizontal-Tail Loads Experienced by a Fighter Airplane in Abrupt Maneuvers
Flight Research Maneuvers Section
June 1944
Primary view of The Use of Geared Spring Tabs for Elevator Control
Phillips, William H.
February 1945
Primary view of A general representation for axial-flow fans and turbines
Perl, W. & Tucker, M.
June 1945
Primary view of An Investigation of a Thermal Ice-Prevention System for a C-46 Cargo Airplane 6: Dry-Air Performance of Thermal System at Several Twin- and Single-Engine Operating Conditions at Various Altitudes
Selna, James & Kees, Harold L.
May 1945
Primary view of An Investigation of Aircraft Heaters 9: Measured and Predicted Performance of Two Exhaust Gas-Air Heat Exchangers and an Apparatus for Evaluating Exhaust Gas-Air Heat Exchangers
Boelter, L. M. K.; Miller, M. A.; Sharp, W. H.; Morrin, E. H.; Iversen, H. W. & Mason, W. E.
March 1943
Primary view of Performance of an exhaust-gas "blowdown" turbine on a nine-cylinder radial engine
Turner, L. Richard & Desmon, Leland G.
December 1944
Primary view of Thermodynamic Design of Double-Panel, Air-Heated Windshields for Ice Prevention
Kushnick, Jerome L.
June 1943
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