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Vibration Surveys of the P-40 Rudder and Fin-Rudder Assembly
Document ID: 19930092907
NTRS Full-Text: Click to View  [PDF Size: 4.8 MB]
Author: Regier, Arthur A
Abstract: No Abstract Available
Publication Year: 1943
Report/Patent Number: NACA-WR-L-652
Date Acquired: Sep 01, 1996
Full-Scale Tunnel Measurements of the Pressures on the Elevator and Fuselage of the Curtiss XP-55 Airplane
Document ID: 19930092704
NTRS Full-Text: Click to View  [PDF Size: 32.5 MB]
Author: Dingeldein, Richard C
Abstract: No Abstract Available
Publication Year: 1943
Report/Patent Number: NACA-WR-L-630
Date Acquired: Sep 01, 1996
Flight Measurements of the Rudder Control and Sideslip Characteristics of Four Vertical Tail Arrangements on the P-40 Series Airplanes
Document ID: 19930092648
NTRS Full-Text: Click to View  [PDF Size: 29.3 MB]
Author: Vensel, Joseph R
Abstract: No Abstract Available
Publication Year: 1942
Report/Patent Number: NACA-WR-L-547
Date Acquired: Sep 01, 1996
Flight Tests of Internally Balanced, Sealed Ailerons on the Curtiss XP-60 Airplane
Document ID: 20160003561
NTRS Full-Text: Click to View  [PDF Size: 5.5 MB]
Author: Gilruth, R. R.
Abstract: Results are presented of brief flight tests of the aileron characteristics of the XP-60 airplane hide
Publication Year: 1942
Document Type: Technical Report
Date Acquired: Mar 23, 2016
An Investigation of the Elements which Contribute to Statical and Dynamical Stability, and of the Effects of Variation in Those Elements
Document ID: 19930091044
NTRS Full-Text: Click to View  [PDF Size: 42.1 MB]
Author: Klemin, Alexander; Warner, Edward P; Denkinger, George M
Abstract: Part 1 gives details of models tested and methods of testing of the Eiffel 36 wing alone and the JN2 hide
Publication Year: 1918
Report/Patent Number: NACA-TR-17
Date Acquired: Sep 01, 1996
Preliminary Flight Research on an All-Movable Horizontal Tail as a Longitudinal Control for Flight at High Mach Numbers
Document ID: 19930092870
NTRS Full-Text: Click to View  [PDF Size: 7.2 MB]
Author: Kleckner, Harold F
Abstract: No Abstract Available
Publication Year: 1945
Report/Patent Number: NACA-WR-L-89, NACA-ARR-L5C08
Date Acquired: Sep 01, 1996
Effects of Propeller Operation and Angle of Yaw on the Distribution of the Load on the Horizontal Tail Surface of a Typical Pursuit Airplane
Document ID: 19930092859
NTRS Full-Text: Click to View  [PDF Size: 27.2 MB]
Author: Dingeldein, Richard C
Abstract: No abstract available
Publication Year: 1944
Document Type: Technical Report
Report/Patent Number: NACA-WR-L-227, NACA-ARR-4B10
Date Acquired: Sep 04, 1996
Flight Investigation of NACA D(sub S) Cowlings on the XP-42 Airplane II : Low-Inlet-Velocity Cowling With Axial-Flow Fan and Propeller Cuffs
Document ID: 19930092650
NTRS Full-Text: Click to View  [PDF Size: 13.9 MB]
Author: Voglewede, T J
Abstract: No Abstract Available
Publication Year: 1943
Report/Patent Number: NACA-WR-L-243
Date Acquired: Sep 01, 1996
Flight Investigation on a Fighter-type Airplane of Factors which Affect the Loads and Load Distributions on the Vertical Tail Surfaces During Rudder Kicks and Fishtails
Document ID: 19930082037
NTRS Full-Text: Click to View  [PDF Size: 40.6 MB]
Author: Boshar, John
Abstract: No Abstract Available
Publication Year: 1947
Report/Patent Number: NACA-TN-1394
Date Acquired: Sep 01, 1996
Measurement of Individual Aileron Hinge Moments and Aileron Control Characteristics of a P-40F Airplane
Document ID: 19930092941
NTRS Full-Text: Click to View  [PDF Size: 29.4 MB]
Author: Goranson, R Fabian
Abstract: No Abstract Available
Publication Year: 1945
Report/Patent Number: NACA-WR-L-649, NACA-MR-L5A29a
Date Acquired: Sep 01, 1996
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