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Primary view of Interference of Wing and Fuselage From Tests of 17 Combinations in the N.A.C.A. Variable-Density Tunnel Combination With Special Junctures
Sherman, Albert
March 1938
Primary view of Quantum interference
Sessler, Andrew M.
January 1, 2004
Primary view of Multilevel Topological Interference Management: A TIM-TIN Perspective
Geng, Chunhua; Sun, Hua & Jafar, Syed A.
August 5, 2021
Primary view of ELECTRONIC INTERFERENCE REDUCTION IN ACOUSTIC EMISSION TESTING.
Davis, T. J.
January 1, 1971
Primary view of INTERFERING RESONANCES.
Moldauer, P.A.
January 1, 1968
Primary view of What can we measure in rho--$omega$ interference experiments
Rabl, A. & Reay, N.W.
January 1, 1972
Primary view of Some Lift and Drag Measurements of a Representative Bomber Nacelle on a Low-Drag Wing 2
Ellis, Macon C., Jr.
September 1942
Primary view of Supersonic wave interference affecting stability
Love, Eugene S.
September 1958
Primary view of A summary of information on support interference at transonic and supersonic speeds
Love, Eugene S.
January 12, 1954
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 Notch Filter Design for Power Line Interference Artifact Reduction of ECG Signal and Feature Extraction in LabVIEW
Kasidi, Divyasri
May 2022
Primary view of Interaction of a Jet and Flat Plate Located in an Airstream
Englert, Gerald W.; Wasserbauer, Joseph F. & Whalen, Paul
September 8, 1955
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
Smith, Norman F. & Carlson, Harry W.
March 11, 1955
Primary view of The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselagestore Configurations 6. - Swept-Wing Heavy-Bomber Configuration With Stores of Different Sizes and Shapes
Smith, Norman F.
March 8, 1956
Primary view of Some Interference Effects That Influence Vertical-Tail Loads at Supersonic Speeds
Edwards, S. Sherman
February 17, 1956
Primary view of Wind-Tunnel Technique for Simultaneous Simulation of External Flow Field About Nacelle Inlet and Exit Airstreams at Supersonic Speeds
Englert, Gerald W. & Luidens, Roger W.
January 1957
Primary view of The Origin and Distribution of Supsonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselage-Store Configurations 5 - Swept-Wing Heavy-Bomber Configuration With Large Store (Nacelle). Mach Number, 2.01
Carlson, Harry W. & Geier, Douglas J.
February 13, 1956
Primary view of The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselage-Store Configurations 4. - Delta-Wing Heavy-Bomber Configuration With Large Store. Mach Number, 1.61
Morris, Odell A.
December 15, 1955
Primary view of The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselage-Store Configurations 3 - Swept-Wing Fighter-Bomber Configuration With Large and Small Stores. Mach Number, 1.61
Smith, Norman F. & Carlson, Harry W.
September 15, 1955
Primary view of Flight Characteristics of a Wingless Rocket- Powered Model With Four Externally Mounted Air-to-Air Missiles at Mach Numbers 0.7 to 1.6
Henning, Allen B. & Brown, Clarence A., Jr.
January 25, 1955
Primary view of Minimum wave drag for arbitrary arrangements of wings and bodies
Jones, Robert T.
February 1956
Primary view of A Wind-Tunnel Investigation of Bomb Release at a Mach Number of 1.62
Rainey, Robert W.
March 19, 1954
Primary view of Ground Effect on Downwash Angles and Wake Location
Katzoff, S. & Sweberg, Harold H.
May 1942
Primary view of The origin and distribution of supersonic store interference from measurement of individual forces on several wing-fuselage-store configurations 3: swept-wing fighter-bomber configuration with large and small stores. Mach number 1.61
Smith, Norman F. & Carlson, Harry W.
September 15, 1955
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