FLIGHT DYNAMICS ERRATA, 1st Edition

• page xvi, URL in third line of last paragraph should be http://www.stengel.mycpanel.princeton.edu. (RS, 3/11/09)
• page 8, "... currently owned and operated by Flight Level Engineering in cooperation with Embry-Riddle Aeronautical University." reference: Croft, J., "Feeling FBW," Aviation Week & Space Technology, May 15-28, 2017, pp. 44-46.
• page 56, Change second sentence to read "With zero sideslip angle, the vertical flight-path angle is ..." (AV, 2/26/08)
• page 58, MATLAB output: xid = 2.8624. (AV, 2/26/08)
• page 62, line 9: rho(z) should be divided by rho-sub-SL. (DM, 11/4/04)
• page 63, eq. 2.3-14b: multiply C-sub-D-sub-alpha by alpha. (IT, 1/21/05)
• page 63, eq. 2.3-16: C-sub-L-sub-alpha^2 should be (C-sub-L-sub-alpha)^2. (IT, 1/21/05)
• page 72, line 6, "eq. 2.4-7" should be "eq. 2.4-8". (ME, 10/20/10)
• page 88, Figure 2.4-9 caption: "movement" should be "moment". (IT, 1/21/05)
• page 90, line 11, change "equation 2.3-20" to "equation 2.3-21". (AJL, 10/11/14)
• page 90, line 14, change "equation 2.2-33" to "equation 2.2-32". (AJL, 10/11/14)
• page 92, Insert C-sub-m-sub-alpha after "forces" on line 6 and remove from line 7. (DL, 7/12/05)
• page 97, 2 lines below eq. 2.4-62: Change S-4 to S-2. (RS, 10/4/10)
• page 109, line 24: co-axial counter-rotating propellers are sometimes called "contra-rotating" propellers. (RK, 2/2/11)
• page 117, eq. 2.5-37: change rho^2 to rho V^2. (DL, 9/23/05)
• page 136, Figure 2.6-5: Horizontal axis should be labeled "Equivalent Airspeed, m/s". (BK, 10/26/16)
• page 179, eq. 3.2-93a and 3.2-93b: add prime to v on left side of equation, following eq. 3.2-91. (DL, 12/12/06)
• page 184-187: Replace discussion of quaternions with material at Quaternions.
• page 187, Below eq. 3.2-121, reference should be made to eq. 3.2-36 rather than 3.2-35. (DL, 5/11/07)
• page 188, eq. 3.2-127: third term on right should be "- (r^2 v+ p^2) delta-y". (JG, 9/2011)
• page 193, line 13: "... and delta g-sub-E contains ..." (DL, 11/10/04)
• page 196, line 9: "eq. 3.2-111 that ..." (DL, 11/10/04)
• page 200, eq. 3.4-1: dot missing over the final "q" in the equation (RS, 10/12/06)
• page 232, eq. 3.5-18: first line, remove term between first and second "=" signs (RS, 3/8/13)
• page 260, line 4: replace "fmins" by "fminsearch" (RS, 11/15/12)
• page 281, "sensitivity". (RS, 11/14/06)
• page 284, line 3: Should be (eq. 4.1-58). (RK, 2/2/11)
• page 291, eq. 4.1-107: F-sub-LD(5,3) should be tan (theta-sub-o); F-sub-LD(6,3) should be sec (theta-sub-o). (RS, 10/24/08)
• page 294, eq. 4.1-125: F-sub-LD(5,3) should be tan (gamma-sub-o); F-sub-LD(6,3) should be sec (gamma-sub-o). (RS, 10/24/08)
• page 348, Figure 4.4-3: caption should be "(a) Amplitude ratio. (b) Phase angle." (RS, 12/1/06)
• page 354, Figure 4.4-7: Labeling of omega-sub-n-sub-SP and z-sub-2 is reversed. Dashed vertical line for z-sub-2 missing on phase angle plot. (RS, 1/19/05)
• page 390, eq. 4.6-2: This is a single integral over z, not a double integral over x and z. Ix = integral(zmin, zmax, x(z)z^2 dz). (RS, 2/14/08)
• page 422, eq. 4.7-2: fraction should be "-(s - 2/tau)/(s + 2/tau). (RS, 9/16/05)
• page 475, eq. 5.2-67: C-sub-L-sub-V should be C-sub-D-sub-V. (RS, 11/14/06)
• page 475, M in numerators of eq. 5.2-68 and 5.2-69 should be M^2. (RS, 12/6/08)
• page 475, eq. 5.2-69: Numerator should be (eta - ...) (RS, 12/6/08)
• page 476, Damping ratios in Table 5.2-3 should be adjusted accordingly. (RS, 12/6/08)
• page 476, eq. 5.2-70: (1 + eta) should be (1 - eta)^(1/2), where eta is less than or equal to 0. (RS, 12/6/08)
• page 481, eq. 5.2-91, change D-sub-L to D-sub-V. (LV, 10/28/14)
• page 482, eq. 5.2-97, change 2nd term to sqrt((g L-sub-V / V-sub-o) (1 - ((V-sub-o / g) (del V-sub-W / del z)))). (LV, 10/28/14)
• page 500, Fig. 5.3-8b, vertical axis: 1 should be 0.1 (RS, 10/23/08)
• page 522, Figure 5.4-5: caption should be "Frequency response of flight path angle (solid line), angle of attack (dashed line), and pitch angle (dashed-dotted line) to sinusoidal thrust input." (RS 12/5/06)
• page 528, Footnote 2: First-order time to double is -0.693 tau, where tau < 0. (RS, 8/16/10)
• page 547, eq. 5.5-51, change C-sub-L-sub-q-hat to C-sub-H-sub-q-hat. (LV, 10-28-14)
• page 569, Reference B-6: the date is 1904 rather than 1903. (RS, 6/19/09)
• page 570, Reference H-4: NACA Report 767. (RS, 6/19/09)
• page 570, Reference L-1: revised title, Aerodynamics: Constituting the First Volume of a Complete Work on Aerial Flight. (RS, 6/19/09)
• page 570, add Reference L-2: Lanchester, F. W., Aerodonetics: Constituting the Second Volume of a Complete Work on Aerial Flight, Arnold Constable, London, 1908. (RS, 6/19/09)
• page 575, eq. 6.1-15: F-sub-LD(4,1) should be tan (gamma-sub-o). (RS, 10/24/08)
• page 580, eq. 6.2-13: "- s" should be "- (N-sub-r + Y-sub-beta / V-sub-zero)s" (RS 12/10/06)
• page 581, lines 6 and 7: re-phrase: "... supersonic speed. The vertical tail's center of pressure may move aft; however, ..." (RK, 12/6/10)
• page 590, eq. 6.3-19, change "+ L-sub-phi" to "- L-sub-phi". (LV, 10-28-14)
• page 597, Table 6.4-1 caption: change "5.4" to 6.4". (RS, 11/30/06)
• page 603, eq. 6.4-38: Add the 1st term of eq. 6.4-37 to the right side of eq. 6.4-38. The 2 equations take the general form, lambda-sub-1,2 = c1 +/- c2, and c1 is missing from eq. 6.4-38 (NK, 6/23/14)
• page 627, next to last line: should be |delta-phi / delta-beta|. (RS 12/13/06)
• page 683, eq. 7.1-6: F-sub-LD(4,3) should be tan (gamma-sub-o). (RS, 10/24/08)
• page 758, eq. 7.4-8, change "cos 2 alpha" to "sin 2 alpha". (LV, 10-28-14)
• page 816, line 9 of computer code: "CLa = 3.141592 * AR/(1 + sqrt(1 + (AR / 2)^2);" (RS, 8/23/05)
• page 834, "Deep (super) stall, 502, 682, 750, 762" (RS, 11/3/14)
• page 844, "Van der Pol oscillator, 734" (RS, 1/3/06)