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keywords:(subsonic wind tunnel)

Synonyms were used for: Subsonic • tunnels • wind
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Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. volume 12. Vertical Tail Net Chordwise Pressure Distributions and Isobars

M. E. Manro / J. P. Moulijn / J. D. Knittel | NTIS | 1972

Keywords: Wind tunnel models , Subsonic flow

Pressure Distributions on a Delta Wing Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 11. Vertical tail section and Total Surface Aerodynamic Coefficients, Chordwise Pressure Distributions

M. E. Manro / J. P. Moulijn / J. D. Knittel | NTIS | 1972

Keywords: Subsonic flow , Wind tunnel models

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 9. Horizontal Stabilzer Section and Total Surface Aerodynamic Coefficients, Chordwise Pressure Distributions

M. E. Manro / J. P. Moulijn / J. D. Knittel | NTIS | 1972

Keywords: Subsonic flow , Wind tunnel models

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 6. Wing Chordwise Pressure Distribution - Nacelles Off

M. E. Manro / J. P. Moulijn / J. D. Knittel | NTIS | 1972

Keywords: Subsonic flow , Wind tunnel models

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 3. Wing Section and Total Surface Aerodynamic Coefficients

M. E. Manro / J. P. Moulijn / J. D. Knittel | NTIS | 1972

Keywords: Wind tunnel models , Subsonic flow

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 4. Wing Chordwise Pressure Distributions - Nacelles on

M. E. Manro / J. P. Moulijn / J. D. Knittel | NTIS | 1972

Keywords: Wind tunnel models , Subsonic flow

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9 Volume 8. Wing Chordwise Pressure Distributions, Effects of: Nacelles, Flaps, Spoilers, Sideslip, and Reynolds Number. Part 1

M. E. Manro / J. P. Moulijn / J. D. Knittel | NTIS | 1972

Keywords: Subsonic flow , Wind tunnel models

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 1. Summary Report

M. E. Manro / J. P. Moulijn / J. D. Knittel | NTIS | 1972

Keywords: Wind tunnel models , Subsonic flow

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 2. Comparisons of Theory and Experiment

M. E. Manro / J. P. Moulijn / J. D. Knittel | NTIS | 1972

Keywords: Wind tunnel models , Subsonic flow