Method for estimating lift interference of wing-body combinations at supersonic speeds Page: 22 of 45
43 p. : ill.View a full description of this report.
Extracted Text
The following text was automatically extracted from the image on this page using optical character recognition software:
NACA RM A51J04
REFERENCES
1. Ferrari, Carlo: Interference Between Wing and Body at Supersonic
Speeds - Theory and Numerical Application. Jour. Aero. Sci.,
vol. 15, no. 6, 1948, pp. 317-336.
2. Nielsen, Jack N., and Matteson, Frederick H.: Calculative Method
for Estimating the Interference Pressure Field at Zero Lift on a
Symmetrical Swept-Back Wing Mounted on a Circular Cylindrical Body.
NACA RM A9E19, 1949.
3. Moskowitz, Barry, and Maslen, Stephen H. : Experimental Pressure
Distributions Over Two Wing-Body Combinations at Mach Number 1.9.
NACA RM ESOJ09, 1951.
4. Morikawa, George: The Wing-Body Problem for Linearized Supersonic
Flow. GALCIT J.P.L. PR 4-116. Dec. 19, 1949.
5. Nielsen, Jack N.: Supersonic Wing-Body Interference.
California Institute of Technology, 1951.
6. Stewart, H. J., and Meghreblian, R. V.: Body-Wing Interference in
Supersonic Flow. GALCIT J.P.L. PR 4-99, June 2, 1949.
7T Morikawa, George: Supersonic Wing-Body Lift. Jour. Aero..Sci.,
vol. 18, no. 4, 1951.
8. Nielsen, Jack N., Katzen, Elliott D., and Tang, Kenneth K.: Lift
and Pitching-Mment Interference Between a Pointed Cylindrical 7
Body and Triangular Wings of Various Aspect Ratios at Mach Numbers
of 1.50 and 2.02. NACA RM A50F06, 1990.
9. Sireiter, John R.: Aerodynamic Properties of Slender Wing-Body
Ccabinations at Subsonic, Transonic, and Supersohic Speeds.
NACA Rep. 962, 1948. (Formerly NACA TN's 1662 and 1897)
10. Jones, Robert T.: Properties of Low-Aspect-Ratio Pointed Wings at
Speeds Below and Above the Speed of Sound. NACA TN 1032, 1946.
11. Beskin, L.: Determination of Upwash Around a Body of Revolution at
Supersonic Velocities. Johns Hopkins Univ. Applied Physics Lab.,
Rept. No. CM-251, 1946.
12. Lagerstrom, P. A., and Van Dyke, M. D.: General Considerations About
Planar and Non-Planar Lifting Systems. Douglas Aircraft Co., Inc.,
Rept. No. SM-13432, 1949.21
Upcoming Pages
Here’s what’s next.
Search Inside
This report can be searched. Note: Results may vary based on the legibility of text within the document.
Tools / Downloads
Get a copy of this page or view the extracted text.
Citing and Sharing
Basic information for referencing this web page. We also provide extended guidance on usage rights, references, copying or embedding.
Reference the current page of this Report.
Nielsen, Jack N. & Kaattari, George E. Method for estimating lift interference of wing-body combinations at supersonic speeds, report, December 31, 1951; (https://digital.library.unt.edu/ark:/67531/metadc59104/m1/22/: accessed May 24, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.