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Wind-tunnel investigation of effect of yaw on lateral-stability characteristics. II, Rectangular N.A.C.A. 23012 wing with a circular fuselage and a fin / by M.J. Bamber and R.O. House.
Connect to full text Available online
View online- Format:
- Book
- Government document
- Author/Creator:
- Bamber, M. J., author.
- House, R. O., author.
- Series:
- Technical note (United States. National Advisory Committee for Aeronautics) ; 730.
- Technical note / National Advisory Committee for Aeronautics ; No. 730
- Language:
- English
- Subjects (All):
- Airplanes--Wings--Testing.
- Airplanes.
- Airplanes--Fuselage.
- Stability of airplanes.
- Rolling (Aerodynamics).
- Yawing (Aerodynamics).
- Wind tunnel testing.
- fuselages.
- Physical Description:
- 1 online resource (9 pages, 11 unnumbered pages) : illustrations.
- Other Title:
- Rectangular N.A.C.A. 23012 wing with a circular fuselage and a fin
- Rectangular National Advisory Committee for Aeronautics 23012 wing with a circular fuselage and a fin
- Place of Publication:
- Washington, [D.C.] : National Advisory Committee for Aeronautics, 1939.
- Summary:
- An N.A.C.A. 23012 rectangular wing with rounded tips was tested in combination with a fuselage of circular cross section at several angles of yaw in the N.A.C.A. 7- by 10-foot wind tunnel. The model was tested as a high-wing, a midwing, and a low-wing monoplane; for each wing location, tests were made with two amounts of dihedral and with partial-span split flaps. For each combination of wing and fuselage, tests were made with and without a fin. Sample charts of the coefficients of rolling moment, yawing moment, and lateral force are given for some of the combinations tested. THe rate of change in the coefficients with angle of yaw is given for stability calculation.
- Notes:
- Description based on online resource, title from title screen (viewed May 29, 2020).
- "September 1939."
- "Langley Memorial Aeronautical Laboratory."
- No Federal Depository Library Program (FDLP) item number.
- Includes bibliographical references (page 9).
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.
- Other Format:
- Print version: Bamber, M. J. Wind-tunnel investigation of effect of yaw on lateral-stability characteristics.
- OCLC:
- 1156323998
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