Effect of Gap on Aerodynamic Characteristics of NACA 0009 Airfoil with 30-Percent-Chord Plain Flap, R. I. SEARS; No. L-380 (Advance Restricted Report Aug 1941) 12 p, 10 supp plates: Large Aerodynamic Balance of Various Nose Shapes With 30-Percent-Chord Flap on NACA 0009 Airfoil, R. I. SEARS and H. P. HOGGARD, Jr; No. L-301 (Advanced Restricted Report Aug 1941) 18 p, 21 supp plates: Small Aerodynamic Balance of Various Nose Shapes Used With 30-Percent-Chord Flap on NACA 0009 Airfoil, M. B. AMES, Jr; No. L-355 (Advance Restricted Report Sept 1941) 14 p, 17 supp plates: Medium Aerodynamic Balance of Various Nose Shapes Used With 30-Percent-Chord Flap on NACA 0009 Airfoil, M. B. AMES, Jr and D. R. EASTMAN, Jr; No. L-464 (Advance Restricted Report Mar 1942) 10 p, 13 supp plates: Use of Beveled Trailing Edge to Reduce Hinge Moment of Control Surface, R. T. JONES and M. B. AMES, Jr; No. L-454 (Advance Restricted Report June 1942) 14 p, 9 supp plates: 30-Percent-Chord Plain Flap on NACA 0015 Airfoil, R. I. SEARS and R. B. LIDDELL; No. L-448 (Advance Restricted Report July 1942) 17 p, 7 supp plates: Medium Aerodynamic Balance of Two Nose Shapes Used with 30-Percent-Chord Flap on NACA 0015 Airfoil, R. I. SEARS and H. P. HOGGARD, Jr; No. L-378 (Advance Restricted Report July 1942) 14 p, 8 supp plates: Large Aerodynamic Balance of Two Nose Shapes Used with 30-Percent-Chord Flap on NACA 0015 Airfoil, R. I. SEARS and C. L. GILLIS; No. L-339 (Advance Restricted Report July 1942) 21 p, 6 supp plates: Some Analytical Considerations and Experimental Test Results for Internally Balanced Flap, R. I. SEARS; No. L-366 (Advance Restricted Report Sept 1942) 12 p. 4 supp plates: A 30-Percent-Chord Plain Flap With Straight Contour on NACA 0015 Airfoil, H. P. HOGGARD, Jr: No. L-447 (Advance Restricted Report Jan 1943) 15 p, 22 supp plates: Various Large Overhand and Internal-Type Aerodynamic Balances for Straight-Contour Flap on NACA 0015 Airfoil, R. I. SEARS and H. P. HOG GARD, Jr; No. L-314 (Advance Confidential Report 3G20 July 1943) 16 p, 13 supp plates: Various Flap Overhangs Used With 30-Percent-Chord Flap on NACA 66-009 Airfoil, C. L. GILLIS and V. E. LOCKWOOD; No. L-290 (Advance Restricted Report n 3F29 June 1943) 18 p, 32 supp plates: NACA 0009 Airfoil With 30-Percent-Chord Double Plain Flap. R. I. SEARS and P. E. PURSER; No. L-205 (Advance Restricted Report L4D03 Apr 1944) 22 p, 48 supp plates: Pressure Distribution Over an NACA 0009 Airfoil with 0.30 Airfoil-Chord Beveled-Trailing-Edge Flaps, H. P. HOGGARD, Jr and M. E. BULLOCH; No. L-350 (Advance Confidential Report 4B28 Feb 1944) 14 p. 45 supp plates: Linked Overhang Aerodynamic Balance, R. I. SEARS and R. B. LIDDELL; No. L-215 (Advance Confidential Report L4F23 June 1944) 16 p. 36 supp plates: Double Flap with Overhand and Internal Aerodynamic Balance, R. B. LIDDELL; No. L-186 (Advance Restricted Report L4I11f Oct 1944) 16 p, 41 supp plates: Plain and Balanced Flaps on NACA 0009 Rectangular Semispan Tail Surface, I. E. GARNER; No. L-175 (Advance Restricted Report L5C01 Mar 1945) 17 p, 33 supp plates: Medium and Large Aerodynamic Balances of Two Nose Shapes and a Plain Overhand Used With a 0.40-Airfoil-Chord Flap on NACA 0009 Airfoil, J. M. RIEBE and O. CHURCH; No. L-196 (Advance Restricted Report L5F06 June 1945) 18 p. 36 supp plates: Medium and Large Aerodynamic Balances of Two Nose Shapes and Plain Overhang Used with 0.20-Airfoil-Chord Flap on NACA 0009 Airfoil, J. M. RIEBE and E. G. McKINNEY. (Advance Restricted Report June 1941)
Wind-tunnel investigation of control-surface characteristics
Nat Advisory Committee Aeronautics -- Wartime Reports
1941
10 pages
16 supp plate
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Wind-tunnel investigation of effect of tab balance on tab and control-surface characteristics
Engineering Index Backfile | 1947
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